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Main repository for the NREL-supported OpenFAST whole-turbine and FAST.Farm wind farm simulation codes.
http://openfast.readthedocs.io
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Nodal Outputs for Elastodyn #1786

Open James-Ilosta opened 9 months ago

James-Ilosta commented 9 months ago

I'm trying to extract nodal outputs at each of the blade stations in Elastodyn, but when I run OpenFAST I get the following warning:

Running ElastoDyn.
Nodal outputs section of ElastoDyn input file not found or improperly formatted.
AD15 Nodal Outputs: Nodal output section of AeroDyn input file not found or improperly formatted.
Skipping nodal outputs.

I had tried looking through the documentation: https://openfast.readthedocs.io/en/dev/source/user/elastodyn/EDNodalOutputs.html https://openfast.readthedocs.io/en/dev/source/user/aerodyn/input.html#ad-nodal-outputs

and as far as I can tell, I have kept the same format as stated inside that page. I also looked at the other issue: https://github.com/OpenFAST/openfast/issues/783

From what I can tell, I don't have an additional line of "---" as this user had.

How would I typically get the nodal values for Elastodyn and Aerodyn? Is there an example I could follow or part of the manual that I have missed?

My Elastodyn and Aerodyn files are listed below:

------- ELASTODYN for OpenFAST INPUT FILE -------------------------------------------
NREL 5.0 MW Baseline Wind Turbine for Use in Offshore Analysis. Properties from Dutch Offshore Wind Energy Converter (DOWEC) 6MW Pre-Design (10046_009.pdf) and REpower 5M 5MW (5m_uk.pdf);
---------------------- SIMULATION CONTROL --------------------------------------
False         Echo        - Echo input data to "<RootName>.ech" (flag)
          3   Method      - Integration method: {1: RK4, 2: AB4, or 3: ABM4} (-)
"default"     DT          - Integration time step (s)
---------------------- DEGREES OF FREEDOM --------------------------------------
True          FlapDOF1    - First flapwise blade mode DOF (flag)
True          FlapDOF2    - Second flapwise blade mode DOF (flag)
True          EdgeDOF     - First edgewise blade mode DOF (flag)
False         TeetDOF     - Rotor-teeter DOF (flag) [unused for 3 blades]
True          DrTrDOF     - Drivetrain rotational-flexibility DOF (flag)
True          GenDOF      - Generator DOF (flag)
True          YawDOF      - Yaw DOF (flag)
True          TwFADOF1    - First fore-aft tower bending-mode DOF (flag)
True          TwFADOF2    - Second fore-aft tower bending-mode DOF (flag)
True          TwSSDOF1    - First side-to-side tower bending-mode DOF (flag)
True          TwSSDOF2    - Second side-to-side tower bending-mode DOF (flag)
True          PtfmSgDOF   - Platform horizontal surge translation DOF (flag)
True          PtfmSwDOF   - Platform horizontal sway translation DOF (flag)
True          PtfmHvDOF   - Platform vertical heave translation DOF (flag)
True          PtfmRDOF    - Platform roll tilt rotation DOF (flag)
True          PtfmPDOF    - Platform pitch tilt rotation DOF (flag)
True          PtfmYDOF    - Platform yaw rotation DOF (flag)
---------------------- INITIAL CONDITIONS --------------------------------------
          0   OoPDefl     - Initial out-of-plane blade-tip displacement (meters)
          0   IPDefl      - Initial in-plane blade-tip deflection (meters)
          0   BlPitch(1)  - Blade 1 initial pitch (degrees)
          0   BlPitch(2)  - Blade 2 initial pitch (degrees)
          0   BlPitch(3)  - Blade 3 initial pitch (degrees) [unused for 2 blades]
          0   TeetDefl    - Initial or fixed teeter angle (degrees) [unused for 3 blades]
          0   Azimuth     - Initial azimuth angle for blade 1 (degrees)
       12.1   RotSpeed    - Initial or fixed rotor speed (rpm)
          0   NacYaw      - Initial or fixed nacelle-yaw angle (degrees)
          0   TTDspFA     - Initial fore-aft tower-top displacement (meters)
          0   TTDspSS     - Initial side-to-side tower-top displacement (meters)
          0   PtfmSurge   - Initial or fixed horizontal surge translational displacement of platform (meters)
          0   PtfmSway    - Initial or fixed horizontal sway translational displacement of platform (meters)
    -0.0009   PtfmHeave   - Initial or fixed vertical heave translational displacement of platform (meters)
          0   PtfmRoll    - Initial or fixed roll tilt rotational displacement of platform (degrees)
          0   PtfmPitch   - Initial or fixed pitch tilt rotational displacement of platform (degrees)
          0   PtfmYaw     - Initial or fixed yaw rotational displacement of platform (degrees)
---------------------- TURBINE CONFIGURATION -----------------------------------
          3   NumBl       - Number of blades (-)
         63   TipRad      - The distance from the rotor apex to the blade tip (meters)
        1.5   HubRad      - The distance from the rotor apex to the blade root (meters)
       -2.5   PreCone(1)  - Blade 1 cone angle (degrees)
       -2.5   PreCone(2)  - Blade 2 cone angle (degrees)
       -2.5   PreCone(3)  - Blade 3 cone angle (degrees) [unused for 2 blades]
          0   HubCM       - Distance from rotor apex to hub mass [positive downwind] (meters)
          0   UndSling    - Undersling length [distance from teeter pin to the rotor apex] (meters) [unused for 3 blades]
          0   Delta3      - Delta-3 angle for teetering rotors (degrees) [unused for 3 blades]
          0   AzimB1Up    - Azimuth value to use for I/O when blade 1 points up (degrees)
    -5.0191   OverHang    - Distance from yaw axis to rotor apex [3 blades] or teeter pin [2 blades] (meters)
      1.912   ShftGagL    - Distance from rotor apex [3 blades] or teeter pin [2 blades] to shaft strain gages [positive for upwind rotors] (meters)
         -5   ShftTilt    - Rotor shaft tilt angle (degrees)
        1.9   NacCMxn     - Downwind distance from the tower-top to the nacelle CM (meters)
          0   NacCMyn     - Lateral  distance from the tower-top to the nacelle CM (meters)
       1.75   NacCMzn     - Vertical distance from the tower-top to the nacelle CM (meters)
   -3.09528   NcIMUxn     - Downwind distance from the tower-top to the nacelle IMU (meters)
          0   NcIMUyn     - Lateral  distance from the tower-top to the nacelle IMU (meters)
    2.23336   NcIMUzn     - Vertical distance from the tower-top to the nacelle IMU (meters)
    1.96256   Twr2Shft    - Vertical distance from the tower-top to the rotor shaft (meters)
       87.6   TowerHt     - Height of tower relative to ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters)
         10   TowerBsHt   - Height of tower base relative to ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters)
          0   PtfmCMxt    - Downwind distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters)
          0   PtfmCMyt    - Lateral distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters)
         10   PtfmCMzt    - Vertical distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters)
         10   PtfmRefzt   - Vertical distance from the ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform reference point (meters)
---------------------- MASS AND INERTIA ----------------------------------------
          0   TipMass(1)  - Tip-brake mass, blade 1 (kg)
          0   TipMass(2)  - Tip-brake mass, blade 2 (kg)
          0   TipMass(3)  - Tip-brake mass, blade 3 (kg) [unused for 2 blades]
      56780   HubMass     - Hub mass (kg)
     115926   HubIner     - Hub inertia about rotor axis [3 blades] or teeter axis [2 blades] (kg m^2)
    534.116   GenIner     - Generator inertia about HSS (kg m^2)
     240000   NacMass     - Nacelle mass (kg)
2.60789E+06   NacYIner    - Nacelle inertia about yaw axis (kg m^2)
          0   YawBrMass   - Yaw bearing mass (kg)
          0   PtfmMass    - Platform mass (kg)
          0   PtfmRIner   - Platform inertia for roll tilt rotation about the platform CM (kg m^2)
          0   PtfmPIner   - Platform inertia for pitch tilt rotation about the platform CM (kg m^2)
  1.534E+06   PtfmYIner   - Platform inertia for yaw rotation about the platform CM (kg m^2)
---------------------- BLADE ---------------------------------------------------
         17   BldNodes    - Number of blade nodes (per blade) used for analysis (-)
"NRELOffshrBsline5MW_Blade.dat"    BldFile(1)  - Name of file containing properties for blade 1 (quoted string)
"NRELOffshrBsline5MW_Blade.dat"    BldFile(2)  - Name of file containing properties for blade 2 (quoted string)
"NRELOffshrBsline5MW_Blade.dat"    BldFile(3)  - Name of file containing properties for blade 3 (quoted string) [unused for 2 blades]
---------------------- ROTOR-TEETER --------------------------------------------
          0   TeetMod     - Rotor-teeter spring/damper model {0: none, 1: standard, 2: user-defined from routine UserTeet} (switch) [unused for 3 blades]
          0   TeetDmpP    - Rotor-teeter damper position (degrees) [used only for 2 blades and when TeetMod=1]
          0   TeetDmp     - Rotor-teeter damping constant (N-m/(rad/s)) [used only for 2 blades and when TeetMod=1]
          0   TeetCDmp    - Rotor-teeter rate-independent Coulomb-damping moment (N-m) [used only for 2 blades and when TeetMod=1]
          0   TeetSStP    - Rotor-teeter soft-stop position (degrees) [used only for 2 blades and when TeetMod=1]
          0   TeetHStP    - Rotor-teeter hard-stop position (degrees) [used only for 2 blades and when TeetMod=1]
          0   TeetSSSp    - Rotor-teeter soft-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1]
          0   TeetHSSp    - Rotor-teeter hard-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1]
---------------------- DRIVETRAIN ----------------------------------------------
        100   GBoxEff     - Gearbox efficiency (%)
         97   GBRatio     - Gearbox ratio (-)
8.67637E+08   DTTorSpr    - Drivetrain torsional spring (N-m/rad)
  6.215E+06   DTTorDmp    - Drivetrain torsional damper (N-m/(rad/s))
---------------------- FURLING -------------------------------------------------
False         Furling     - Read in additional model properties for furling turbine (flag) [must currently be FALSE)
"unused"      FurlFile    - Name of file containing furling properties (quoted string) [unused when Furling=False]
---------------------- TOWER ---------------------------------------------------
         20   TwrNodes    - Number of tower nodes used for analysis (-)
"NRELOffshrBsline5MW_OC3Monopile_ElastoDyn_Tower.dat"    TwrFile     - Name of file containing tower properties (quoted string)
---------------------- OUTPUT --------------------------------------------------
True          SumPrint    - Print summary data to "<RootName>.sum" (flag)
          1   OutFile     - Switch to determine where output will be placed: {1: in module output file only; 2: in glue code output file only; 3: both} (currently unused)
True          TabDelim    - Use tab delimiters in text tabular output file? (flag) (currently unused)
"ES10.3E2"    OutFmt      - Format used for text tabular output (except time).  Resulting field should be 10 characters. (quoted string) (currently unused)
          0   TStart      - Time to begin tabular output (s) (currently unused)
          1   DecFact     - Decimation factor for tabular output {1: output every time step} (-) (currently unused)
          1   NTwGages    - Number of tower nodes that have strain gages for output [0 to 9] (-)
         20   TwrGagNd    - List of tower nodes that have strain gages [1 to TwrNodes] (-) [unused if NTwGages=0]
          3   NBlGages    - Number of blade nodes that have strain gages for output [0 to 9] (-)
          5,          9,         13    BldGagNd    - List of blade nodes that have strain gages [1 to BldNodes] (-) [unused if NBlGages=0]
              OutList     - The next line(s) contains a list of output parameters.  See OutListParameters.xlsx for a listing of available output channels, (-)
"OoPDefl1, IPDefl1, TwstDefl1"    - Blade 1 out-of-plane and in-plane deflections and tip twist
"BldPitch1"                       - Blade 1 pitch angle
"Azimuth"                         - Blade 1 azimuth angle
"RotSpeed, GenSpeed"              - Low-speed shaft and high-speed shaft speeds
"TwHt1TPxi, TwHt1TPyi, TTDspTwst" - Tower fore-aft and side-to-side displacements and top twist
"PtfmSurge, PtfmSway"             - Platform horizontal surge displacement
"PtfmRoll , PtfmPitch"            - Platform rotational displacements
"Spn2MLxb1, Spn2MLyb1"            - Blade 1 local edgewise and flapwise bending moments at span station 2 (approx. 50% span)
"RootFxc1, RootFyc1, RootFzc1"    - Out-of-plane shear, in-plane shear, and axial forces at the root of blade 1
"RootMxc1, RootMyc1, RootMzc1"    - In-plane bending, out-of-plane bending, and pitching moments at the root of blade 1
"RotTorq, LSSGagMya, LSSGagMza"   - Rotor torque and low-speed shaft 0- and 90-bending moments at the main bearing
"YawBrFxp, YawBrFyp, YawBrFzp"    - Fore-aft shear, side-to-side shear, and vertical forces at the top of the tower (not rotating with nacelle yaw)
"YawBrMxp, YawBrMyp, YawBrMzp"    - Side-to-side bending, fore-aft bending, and yaw moments at the top of the tower (not rotating with nacelle yaw)
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
----------------------------------- NODE OUTPUTS -------------------------------------------------------------------
    1             BldNd_BladesOut     - Number of blades to output all node information at.  Up to number of blades on turbine. (-)
   50             BldNd_BlOutNd       - Future feature will allow selecting a portion of the nodes to output.  Not implemented yet. (-)
                  OutList             - The next line(s) contains a list of output parameters.  See OutListParameters.xlsx for a listing of available output channels, (-)
"TDx"
"TDy"
"TDz"
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)

Aerodyn File:

------- AERODYN v15 for OpenFAST INPUT FILE -----------------------------------------------
NREL 5.0 MW offshore baseline aerodynamic input properties, with OC3 Monopile tower
======  General Options  ============================================================================
False         Echo               - Echo the input to "<rootname>.AD.ech"?  (flag)
"default"     DTAero             - Time interval for aerodynamic calculations {or "default"} (s)
          1   WakeMod            - Type of wake/induction model (switch) {0=none, 1=BEMT, 2=DBEMT, 3=OLAF} [WakeMod cannot be 2 or 3 when linearizing]
          2   AFAeroMod          - Type of blade airfoil aerodynamics model (switch) {1=steady model, 2=Beddoes-Leishman unsteady model} [AFAeroMod must be 1 when linearizing]
          1   TwrPotent          - Type tower influence on wind based on potential flow around the tower (switch) {0=none, 1=baseline potential flow, 2=potential flow with Bak correction}
          0   TwrShadow          - Calculate tower influence on wind based on downstream tower shadow (switch) {0=none, 1=Powles model, 2=Eames model}
True          TwrAero            - Calculate tower aerodynamic loads? (flag)
False         FrozenWake         - Assume frozen wake during linearization? (flag) [used only when WakeMod=1 and when linearizing]
False         CavitCheck         - Perform cavitation check? (flag) [AFAeroMod must be 1 when CavitCheck=true]
False         Buoyancy           - Include buoyancy effects? (flag)
False         CompAA             - Flag to compute AeroAcoustics calculation [used only when WakeMod = 1 or 2]
"unused"      AA_InputFile       - AeroAcoustics input file [used only when CompAA=true]
======  Environmental Conditions  ===================================================================
"default"     AirDens            - Air density (kg/m^3)
"default"     KinVisc            - Kinematic viscosity of working fluid (m^2/s)
"default"     SpdSound           - Speed of sound in working fluid (m/s)
"default"     Patm               - Atmospheric pressure (Pa) [used only when CavitCheck=True]
"default"     Pvap               - Vapour pressure of working fluid (Pa) [used only when CavitCheck=True]
======  Blade-Element/Momentum Theory Options  ====================================================== [unused when WakeMod=0 or 3]
          2   SkewMod            - Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [unused when WakeMod=0 or 3]
"default"     SkewModFactor      - Constant used in Pitt/Peters skewed wake model {or "default" is 15/32*pi} (-) [used only when SkewMod=2; unused when WakeMod=0 or 3]
True          TipLoss            - Use the Prandtl tip-loss model? (flag) [unused when WakeMod=0 or 3]
True          HubLoss            - Use the Prandtl hub-loss model? (flag) [unused when WakeMod=0 or 3]
True          TanInd             - Include tangential induction in BEMT calculations? (flag) [unused when WakeMod=0 or 3]
False         AIDrag             - Include the drag term in the axial-induction calculation? (flag) [unused when WakeMod=0 or 3]
False         TIDrag             - Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod=0,3 or TanInd=FALSE]
"Default"     IndToler           - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when WakeMod=0 or 3]
        100   MaxIter            - Maximum number of iteration steps (-) [unused when WakeMod=0]
======  Dynamic Blade-Element/Momentum Theory Options  ============================================== [used only when WakeMod=2]
          2   DBEMT_Mod          - Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1, 3=constant tau1 with continuous formulation} (-) [used only when WakeMod=2]
          4   tau1_const         - Time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1 or 3]
======  OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options  ================== [used only when WakeMod=3]
"unused"      OLAFInputFileName  - Input file for OLAF [used only when WakeMod=3]
======  Beddoes-Leishman Unsteady Airfoil Aerodynamics Options  ===================================== [used only when AFAeroMod=2]
          3   UAMod              - Unsteady Aero Model Switch (switch) {2=B-L Gonzalez, 3=B-L Minnema/Pierce, 4=B-L HGM 4-states, 5=B-L 5 states, 6=Oye, 7=Boeing-Vertol} [used only when AFAeroMod=2]
True          FLookup            - Flag to indicate whether a lookup for f' will be calculated (TRUE) or whether best-fit exponential equations will be used (FALSE); if FALSE S1-S4 must be provided in airfoil input files (flag) [used only when AFAeroMod=2]
======  Airfoil Information =========================================================================
          1   AFTabMod           - Interpolation method for multiple airfoil tables {1=1D interpolation on AoA (first table only); 2=2D interpolation on AoA and Re; 3=2D interpolation on AoA and UserProp} (-)
          1   InCol_Alfa         - The column in the airfoil tables that contains the angle of attack (-)
          2   InCol_Cl           - The column in the airfoil tables that contains the lift coefficient (-)
          3   InCol_Cd           - The column in the airfoil tables that contains the drag coefficient (-)
          4   InCol_Cm           - The column in the airfoil tables that contains the pitching-moment coefficient; use zero if there is no Cm column (-)
          0   InCol_Cpmin        - The column in the airfoil tables that contains the Cpmin coefficient; use zero if there is no Cpmin column (-)
          8   NumAFfiles         - Number of airfoil files used (-)
"Airfoils/Cylinder1.dat"    AFNames            - Airfoil file names (NumAFfiles lines) (quoted strings)
"Airfoils/Cylinder2.dat"
"Airfoils/DU40_A17.dat"
"Airfoils/DU35_A17.dat"
"Airfoils/DU30_A17.dat"
"Airfoils/DU25_A17.dat"
"Airfoils/DU21_A17.dat"
"Airfoils/NACA64_A17.dat"
======  Rotor/Blade Properties  =====================================================================
True          UseBlCm            - Include aerodynamic pitching moment in calculations?  (flag)
"NRELOffshrBsline5MW_AeroDyn_blade.dat"    ADBlFile(1)        - Name of file containing distributed aerodynamic properties for Blade #1 (-)
"NRELOffshrBsline5MW_AeroDyn_blade.dat"    ADBlFile(2)        - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2]
"NRELOffshrBsline5MW_AeroDyn_blade.dat"    ADBlFile(3)        - Name of file containing distributed aerodynamic properties for Blade #3 (-) [unused if NumBl < 3]
======  Hub Properties ============================================================================== [used only when Buoyancy=True]
0.0   VolHub             - Hub volume (m^3)
0.0   HubCenBx           - Hub center of buoyancy x direction offset (m)
======  Nacelle Properties ========================================================================== [used only when Buoyancy=True]
0.0   VolNac             - Nacelle volume (m^3)
0,0,0 NacCenB            - Position of nacelle center of buoyancy from yaw bearing in nacelle coordinates (m)
======  Tail fin Aerodynamics ======================================================================== 
False         TFinAero           - Calculate tail fin aerodynamics model (flag)
"unused"      TFinFile           - Input file for tail fin aerodynamics [used only when TFinAero=True]
======  Tower Influence and Aerodynamics ============================================================ [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True]
         11   NumTwrNds         - Number of tower nodes used in the analysis  (-) [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True]
TwrElev        TwrDiam        TwrCd          TwrTI          TwrCb !TwrTI used only with TwrShadow=2, TwrCb used only with Buoyancy=True
(m)              (m)           (-)            (-)           (-)
1.0000000E+01  6.0000000E+00  1.0000000E+00  1.0000000E-01  0.0
1.7760000E+01  5.7870000E+00  1.0000000E+00  1.0000000E-01  0.0
2.5520000E+01  5.5740000E+00  1.0000000E+00  1.0000000E-01  0.0
3.3280000E+01  5.3610000E+00  1.0000000E+00  1.0000000E-01  0.0
4.1040000E+01  5.1480000E+00  1.0000000E+00  1.0000000E-01  0.0
4.8800000E+01  4.9350000E+00  1.0000000E+00  1.0000000E-01  0.0
5.6560000E+01  4.7220000E+00  1.0000000E+00  1.0000000E-01  0.0
6.4320000E+01  4.5090000E+00  1.0000000E+00  1.0000000E-01  0.0
7.2080000E+01  4.2960000E+00  1.0000000E+00  1.0000000E-01  0.0
7.9840000E+01  4.0830000E+00  1.0000000E+00  1.0000000E-01  0.0
8.7600000E+01  3.8700000E+00  1.0000000E+00  1.0000000E-01  0.0
======  Outputs  ====================================================================================
True          SumPrint            - Generate a summary file listing input options and interpolated properties to "<rootname>.AD.sum"?  (flag)
          0   NBlOuts             - Number of blade node outputs [0 - 9] (-)
          2,          9,         16,          4,          5,          7,         11,         13,         14    BlOutNd             - Blade nodes whose values will be output  (-)
          0   NTwOuts             - Number of tower node outputs [0 - 9]  (-)
          1,          2,          3,          4,          5    TwOutNd             - Tower nodes whose values will be output  (-)
                   OutList             - The next line(s) contains a list of output parameters.  See OutListParameters.xlsx for a listing of available output channels, (-)
"RtAeroFxh, RtAeroFyh, RtAeroFzh"  
"RtAeroMxh, RtAeroMyh, RtAeroMzh"  
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
---------------------- NODE OUTPUTS --------------------------------------------
          3   BldNd_BladesOut  - Blades to output
         99   BldNd_BlOutNd   - Blade nodes on each blade (currently unused)
              OutList     - The next line(s) contains a list of output parameters.  See OutListParameters.xlsx, AeroDyn_Nodes tab for a listing of available output channels, (-)
"Cl"        - Lift force coefficient at each node
"Cd"        - Drag force coefficient at each node
"Cm"        - Pitching moment coefficient at each node

I've also checked the .out file and can't see any node outputs from either Aerodyn or Elastodyn.

jjonkman commented 9 months ago

Dear @James-Ilosta,

Can you enable the Echo option in ElastoDyn and AeroDyn and share the resulting Echo file? Do these files provide any clue as to the issue?

You can find example AeroDyn files with the nodal outputs in the module-level r-test for AeroDyn: https://github.com/OpenFAST/r-test/tree/main/modules/aerodyn.

Best regards

andrew-platt commented 9 months ago

@James-Ilosta, which version of OpenFAST are your running?

James-Ilosta commented 9 months ago

Hi,

I tried the R-test module and the output didn't change. Interestingly, it seems as though the echo files don't contain the node outputs as stated in the input files. Here are the echo files after modifying the AeroDyn File.

Here are the echo files:


This file of echoed input was generated by OpenFAST on 28-Sep-2023 at 12:26:14.

Data from OpenFAST primary input file "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\t1.fst":

               FTitle         - File Header: File Description (line 2)
  "Generated with AeroElasticSE FAST driver"

            T  Echo           - Echo input data to <RootName>.ech (flag)
               AbortLevel     - Error level when simulation should abort (string)
  "FATAL"
   5.0000E+00  TMax           - Total run time (s)
   5.0000E-03  DT             - Recommended module time step (s)
            2  InterpOrder    - Interpolation order for inputs and outputs {0=nearest neighbor ,1=linear, 2=quadratic} (-)
            0  NumCrctn       - Number of corrections{0=explicit calculation, i.e., no corrections} (-)
   9.9999E+04  DT_UJac        - Time between calls to get Jacobians (s)
   1.0000E+06  UJacSclFact    - Scaling factor used in Jacobians (-)

            1  CompElast      - Compute structural dynamics (switch) {1=ElastoDyn; 2=ElastoDyn + BeamDyn for blades}
            1  CompInflow     - inflow wind velocities (switch) {0=still air; 1=InflowWind}
            2  CompAero       - Compute aerodynamic loads (switch) {0=None; 1=AeroDyn}
            1  CompServo      - Compute control and electrical-drive dynamics (switch) {0=None; 1=ServoDyn}
            0  CompHydro      - Compute hydrodynamic loads (switch) {0=None; 1=HydroDyn}
            1  CompSub        - Compute sub-structural dynamics (switch) {0=None; 1=SubDyn}
            0  CompMooring    - Compute mooring system (switch) {0=None; 1=MAP; 2=FEAMooring; 3=MoorDyn; 4=OrcaFlex}
            0  CompIce        - Compute ice loads (switch) {0=None; 1=IceFloe}
            0  MHK            - MHK turbine type (switch) {0=Not an MHK turbine; 1=Fixed MHK turbine; 2=Floating MHK turbine}

   9.8067E+00  Gravity        - Gravitational acceleration (m/s^2)
   1.2250E+00  AirDens        - Air density (kg/m^3)
   1.0270E+03  WtrDens        - Water density (kg/m^3)
   1.4640E-05  KinVisc        - Kinematic viscosity of working fluid (m^2/s)
   3.3500E+02  SpdSound       - Speed of sound in working fluid (m/s)
   1.0350E+05  Patm           - Atmospheric pressure (Pa)
   1.7000E+03  Pvap           - Vapour pressure of working fluid (Pa)
   2.0000E+01  WtrDpth        - Water depth (m)
   0.0000E+00  MSL2SWL        - Offset between still-water level and mean sea level (m)

               EDFile         - Name of file containing ElastoDyn input parameters (-)
  "t1_ElastoDyn.dat"
               BDBldFile(1)   - Name of file containing BeamDyn blade 1input parameters (-)
  "NRELOffshrBsline5MW_BeamDyn.dat"
               BDBldFile(2)   - Name of file containing BeamDyn blade 2input parameters (-)
  "NRELOffshrBsline5MW_BeamDyn.dat"
               BDBldFile(3)   - Name of file containing BeamDyn blade 3input parameters (-)
  "NRELOffshrBsline5MW_BeamDyn.dat"
               InflowFile     - Name of file containing inflow wind input parameters (-)
  "t1_InflowFile.dat"
               AeroFile       - Name of file containing aerodynamic input parameters (-)
  "t1_AeroDyn15.dat"
               ServoFile      - Name of file containing control and electrical-drive input parameters (-)
  "t1_ServoDyn.dat"
               HydroFile      - Name of file containing hydrodynamic input parameters (-)
  "NRELOffshrBsline5MW_OC3Monopile_HydroDyn.dat"
               SubFile        - Name of file containing sub-structural input parameters (-)
  "t1_SubDyn.dat"
               MooringFile    - Name of file containing mooring system input parameters (-)
  "unused"
               IceFile        - Name of file containing ice input parameters (-)
  "unused"

            T  SumPrint       - Print summary data to <RootName>.sum (flag)
   1.0000E+00  SttsTime       - Amount of time between screen status messages (s)
   9.9999E+04  ChkptTime      - Amount of time between creating checkpoint files for potential restart (s)
               DT_Out         - Time step for tabular output (s)
  "0.05"
   0.0000E+00  TStart         - Time to begin tabular output (s)
            1  OutFileFmt     - Format for tabular (time-marching) output file(s) {0: uncompressed binary and text file, 1: text file [<RootName>.out], 2: compressed binary file [<RootName>.outb], 3: both text and compressed binary, 4: uncompressed binary <RootName>.outb]; add for combinations) (-)
            T  TabDelim       - Use tab delimiters in text tabular output file? (flag)
               OutFmt         - Format used for text tabular output (except time).  Resulting field should be 10 characters. (-)
  "ES10.3E2"

            F  Linearize      - Linearization analysis (flag)
            F  CalcSteady     - Calculate a steady-state periodic operating point before linearization? (flag)
            3  TrimCase       - Controller parameter to be trimmed {1:yaw; 2:torque; 3:pitch} (-)
   1.0000E-03  TrimTol        - Tolerance for the rotational speed convergence (-)
   1.0000E-02  TrimGain       - Proportional gain for the rotational speed error (>0) (rad/(rad/s) for yaw or pitch; Nm/(rad/s) for torque)
   0.0000E+00  Twr_Kdmp       - Damping factor for the tower (N/(m/s))
   0.0000E+00  Bld_Kdmp       - Damping factor for the blades (N/(m/s))
            2  NLinTimes      - Number of times to linearize (-) [>=1]

            1  LinInputs      - Include inputs in linearization (switch) {0=none; 1=standard; 2=all module inputs (debug)}
            1  LinOutputs     - Include outputs in linearization (switch) (0=none; 1=from OutList(s); 2=all module outputs (debug))
            F  LinOutJac      - Include full Jacabians in linearization output (for debug) (flag)
            F  LinOutMod      - Write module-level linearization output files in addition to output for full system? (flag)

            0  WrVTK          - Write VTK visualization files (0=none; 1=initialization data only; 2=animation; 3=mode shapes)
            3  VTK_Type       - Type of  VTK visualization data: (1=surfaces; 2=basic meshes (lines/points); 3=all meshes)
            F  VTK_fields     - Write mesh fields to VTK data files? (flag)
   1.5000E+01  VTK_fps        - Frame rate for VTK output(fps)

This file of echoed input was generated by ElastoDyn on 28-Sep-2023 at 12:26:14.

Data from ElastoDyn primary input file "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\t1_ElastoDyn.dat":

               FTitle         - File Header: File Description (line 2)
  "Generated with AeroElasticSE FAST driver"

            T  Echo           - Echo switch
            3  Method         - Requested integration method for ElastoDyn {1: RK4, 2: AB4, or 3: ABM4}
               DT             - Requested integration time for ElastoDyn (seconds)
  "default"

            T  FlapDOF1       - First flapwise blade mode DOF (flag)
            T  FlapDOF2       - Second flapwise blade mode DOF (flag)
            T  EdgeDOF        - Edgewise blade mode DOF (flag)
            F  TeetDOF        - Rotor-teeter DOF (flag)
            T  DrTrDOF        - Drivetrain rotational-flexibility DOF (flag)
            T  GenDOF         - Generator DOF (flag)
            T  YawDOF         - Nacelle-yaw DOF (flag)
            T  TwFADOF1       - First tower fore-aft bending-mode DOF (flag)
            T  TwFADOF2       - Second tower fore-aft bending-mode DOF (flag)
            T  TwSSDOF1       - First tower side-to-side bending-mode DOF (flag)
            T  TwSSDOF2       - Second tower side-to-side bending-mode DOF (flag)
            T  PtfmSgDOF      - Platform horizontal surge translation DOF (flag)
            T  PtfmSwDOF      - Platform horizontal sway translation DOF (flag)
            T  PtfmHvDOF      - Platform vertical heave translation DOF (flag)
            T  PtfmRDOF       - Platform roll tilt rotation DOF (flag)
            T  PtfmPDOF       - Platform pitch tilt rotation DOF (flag)
            T  PtfmYDOF       - Platform yaw rotation DOF (flag)

   0.0000E+00  OoPDefl        - Initial out-of-plane blade-tip displacement (meters)
   0.0000E+00  IPDefl         - Initial in-plane blade-tip deflection (meters)
   0.0000E+00  BlPitch(1)     - Initial blade pitch angles (deg)
   0.0000E+00  BlPitch(2)     - Initial blade pitch angles (deg)
   0.0000E+00  BlPitch(3)     - Initial blade pitch angles (deg)
   0.0000E+00  TeetDefl       - Initial teeter angle (deg)
   0.0000E+00  Azimuth        - Initial azimuth angle for blade 1 (degrees)
   1.2100E+01  RotSpeed       - Initial rotor speed (RPM)
   0.0000E+00  NacYaw         - Initial nacelle-yaw angle (deg)
   0.0000E+00  TTDspFA        - Initial fore-aft tower-top displacement (meters)
   0.0000E+00  TTDspSS        - Initial side-to-side tower-top displacement (meters)
   0.0000E+00  PtfmSurge      - Initial horizontal surge translational displacement of platform (meters)
   0.0000E+00  PtfmSway       - Initial horizontal sway translational displacement of platform (meters)
  -9.0000E-04  PtfmHeave      - Initial vertical heave translational displacement of platform (meters)
   0.0000E+00  PtfmRoll       - Initial roll tilt rotational displacement of platform (deg)
   0.0000E+00  PtfmPitch      - Initial pitch tilt rotational displacement of platform (deg)
   0.0000E+00  PtfmYaw        - Initial yaw rotational displacement of platform (deg)

            3  NumBl          - Number of blades (-)
   6.3000E+01  TipRad         - Preconed blade-tip radius (distance from the rotor apex to the blade tip) (meters)
   1.5000E+00  HubRad         - Preconed hub radius (distance from the rotor apex to the blade root) (meters)
  -2.5000E+00  PreCone(1)     - Rotor precone angles (deg)
  -2.5000E+00  PreCone(2)     - Rotor precone angles (deg)
  -2.5000E+00  PreCone(3)     - Rotor precone angles (deg)
   0.0000E+00  HubCM          - Distance from rotor apex to hub mass (meters)
   0.0000E+00  UndSling       - Undersling length (meters)
   0.0000E+00  Delta3         - Delta-3 angle for teetering rotors (deg)
   0.0000E+00  AzimB1Up       - Azimuth value to use for I/O when blade 1 points up (degrees)
  -5.0191E+00  OverHang       - Distance from yaw axis to rotor apex or teeter pin (meters)
   1.9120E+00  ShftGagL       - Distance from hub or teeter pin to shaft strain gages (meters)
  -5.0000E+00  ShftTilt       - Rotor shaft tilt angle (deg)
   1.9000E+00  NacCMxn        - Downwind distance from tower-top to nacelle CM (meters)
   0.0000E+00  NacCMyn        - Lateral distance from tower-top to nacelle CM (meters)
   1.7500E+00  NacCMzn        - Vertical distance from tower-top to nacelle CM (meters)
  -3.0953E+00  NcIMUxn        - Downwind distance from the tower-top to the nacelle IMU (meters)
   0.0000E+00  NcIMUyn        - Lateral distance from the tower-top to the nacelle IMU (meters)
   2.2334E+00  NcIMUzn        - Vertical distance from the tower-top to the nacelle IMU (meters)
   1.9626E+00  Twr2Shft       - Vertical distance from the tower-top to the rotor shaft (meters)
   8.7600E+01  TowerHt        - Height of tower above ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters)
   1.0000E+01  TowerBsHt      - Height of tower base above ground level [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] (meters)
   0.0000E+00  PtfmCMxt       - Downwind distance from the ground [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters)
   0.0000E+00  PtfmCMyt       - Lateral distance from the ground [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters)
   1.0000E+01  PtfmCMzt       - Vertical distance from the ground [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform CM (meters)
   1.0000E+01  PtfmRefzt      - Vertical distance from the ground [onshore], MSL [offshore wind or floating MHK], or seabed [fixed MHK] to the platform reference point (meters)

   0.0000E+00  TipMass(1)     - Tip-brake masses (kg)
   0.0000E+00  TipMass(2)     - Tip-brake masses (kg)
   0.0000E+00  TipMass(3)     - Tip-brake masses (kg)
   5.6780E+04  HubMass        - Hub mass (kg)
   1.1593E+05  HubIner        - Hub inertia about teeter axis (2-blader) or rotor axis (3-blader) (kg m^2)
   5.3412E+02  GenIner        - Generator inertia about HSS (kg m^2)
   2.4000E+05  NacMass        - Nacelle mass (kg)
   2.6079E+06  NacYIner       - Nacelle yaw inertia (kg m^2)
   0.0000E+00  YawBrMass      - Yaw bearing mass (kg)
   0.0000E+00  PtfmMass       - Platform mass (kg)
   0.0000E+00  PtfmRIner      - Platform inertia for roll tilt rotation about the platform CM (kg m^2)
   0.0000E+00  PtfmPIner      - Platform inertia for pitch tilt rotation about the platform CM (kg m^2)
   1.5340E+06  PtfmYIner      - Platform inertia for yaw rotation about the platform CM (kg m^2)

   1.7000E+01  BldNodes       - Number of blade nodes (per blade) used for analysis (-)
               BldFile(1)     - Name of the file containing properties for blade 1
  "t1_ElastoDyn_blade.dat"
               BldFile(2)     - Name of the file containing properties for blade 2
  "t1_ElastoDyn_blade.dat"
               BldFile(3)     - Name of the file containing properties for blade 3
  "t1_ElastoDyn_blade.dat"

            0  TeetMod        - Rotor-teeter spring/damper model switch (-)
   0.0000E+00  TeetDmpP       - Rotor-teeter damper position (deg)
   0.0000E+00  TeetDmp        - Rotor-teeter damping constant (N-m/(rad/s))
   0.0000E+00  TeetCDmp       - Rotor-teeter rate-independent Coulomb-damping (N-m)
   0.0000E+00  TeetSStP       - Rotor-teeter soft-stop position (deg)
   0.0000E+00  TeetHStP       - Rotor-teeter hard-stop position (deg)
   0.0000E+00  TeetSSSp       - Rotor-teeter soft-stop linear-spring constant (N-m/rad)
   0.0000E+00  TeetHSSp       - Rotor-teeter hard-stop linear-spring constant (N-m/rad)

   1.0000E+02  GBoxEff        - Gearbox efficiency (%)
   9.7000E+01  GBRatio        - Gearbox ratio (-)
   8.6764E+08  DTTorSpr       - Drivetrain torsional spring (N-m/rad)
   6.2150E+06  DTTorDmp       - Drivetrain torsional damper (N-m/(rad/s))

            F  Furling        - Use Additional Furling parameters? (flag)
               FurlFile       - Name of the file containing furling parameters
  "unused"

           20  TwrNodes       - Number of tower nodes used in the analysis (-)
               TwrFile        - Name of the file containing tower properties
  "t1_ElastoDyn_tower.dat"

            T  SumPrint       - Print summary data to <RootName>.sum (flag)
            1  OutFile        - Switch to determine where output will be placed: (1: in module output file only; 2: in glue code output file only; 3: both) (-)
            T  TabDelim       - Flag to cause tab-delimited text output (delimited by space otherwise) (flag)
               OutFmt         - Format used for module's text tabular output (except time); resulting field should be 10 characters (-)
  "ES10.3E2"
   0.0000E+00  Tstart         - Time to start module's tabular output (seconds)
            1  DecFact        - Decimation factor for module's tabular output (1=output every step) (-)
            1  NTwGages       - Number of tower strain gages (-)
               TwrGagNd       - Nodes closest to the tower strain gages (-)
           20
            3  NBlGages       - Number of blade strain gages (-)
               BldGagNd       - Nodes closest to the blade strain gages (-)
            5            9           13

               OutList        - List of user-requested output channels
  "Azimuth"
               OutList        - List of user-requested output channels
  "BldPitch1"
               OutList        - List of user-requested output channels
  "BldPitch2"
               OutList        - List of user-requested output channels
  "BldPitch3"
               OutList        - List of user-requested output channels
  "GenSpeed"
               OutList        - List of user-requested output channels
  "IPDefl1"
               OutList        - List of user-requested output channels
  "LSSGagMya"
               OutList        - List of user-requested output channels
  "LSSGagMza"
               OutList        - List of user-requested output channels
  "OoPDefl1"
               OutList        - List of user-requested output channels
  "PtfmPitch"
               OutList        - List of user-requested output channels
  "PtfmRoll"
               OutList        - List of user-requested output channels
  "PtfmSurge"
               OutList        - List of user-requested output channels
  "PtfmSway"
               OutList        - List of user-requested output channels
  "RootFxc1"
               OutList        - List of user-requested output channels
  "RootFyc1"
               OutList        - List of user-requested output channels
  "RootFzc1"
               OutList        - List of user-requested output channels
  "RootMxc1"
               OutList        - List of user-requested output channels
  "RootMyc1"
               OutList        - List of user-requested output channels
  "RootMzc1"
               OutList        - List of user-requested output channels
  "RotSpeed"
               OutList        - List of user-requested output channels
  "RotTorq"
               OutList        - List of user-requested output channels
  "Spn2MLxb1"
               OutList        - List of user-requested output channels
  "Spn2MLyb1"
               OutList        - List of user-requested output channels
  "Spn9MLzb3"
               OutList        - List of user-requested output channels
  "TTDspTwst"
               OutList        - List of user-requested output channels
  "TwHt1TPxi"
               OutList        - List of user-requested output channels
  "TwHt1TPyi"
               OutList        - List of user-requested output channels
  "TwstDefl1"
               OutList        - List of user-requested output channels
  "YawBrFxp"
               OutList        - List of user-requested output channels
  "YawBrFyp"
               OutList        - List of user-requested output channels
  "YawBrFzp"
               OutList        - List of user-requested output channels
  "YawBrMxp"
               OutList        - List of user-requested output channels
  "YawBrMyp"
               OutList        - List of user-requested output channels
  "YawBrMzp"
               OutList        - List of user-requested output channels
  "END"

Blade 1 input data from file "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\t1_ElastoDyn_blade.dat":

           49  NBlInpSt       - Number of blade input stations
   4.7747E-01  BldFlDmp(1)    - Blade structural damping ratios in flapwise direction
   4.7747E-01  BldFlDmp(2)    - Blade structural damping ratios in flapwise direction
   4.7747E-01  BldEdDmp(1)    - Blade structural damping ratios in edgewise direction

   1.0000E+00  FlStTunr(1)    - Blade flapwise modal stiffness tuners
   1.0000E+00  FlStTunr(2)    - Blade flapwise modal stiffness tuners
   1.0454E+00  AdjBlMs        - Factor to adjust blade mass density
   1.0000E+00  AdjFlSt        - Factor to adjust blade flap stiffness
   1.0000E+00  AdjEdSt        - Factor to adjust blade edge stiffness

               Line1          - Blade input station table
   0.0000E+00   2.5000E-01   1.3308E+01   6.7893E+02   1.8110E+10   1.8114E+10
               Line2          - Blade input station table
   3.2500E-03   2.5000E-01   1.3308E+01   6.7893E+02   1.8110E+10   1.8114E+10
               Line3          - Blade input station table
   1.9510E-02   2.5049E-01   1.3308E+01   7.7336E+02   1.9425E+10   1.9559E+10
               Line4          - Blade input station table
   3.5770E-02   2.5490E-01   1.3308E+01   7.4055E+02   1.7456E+10   1.9498E+10
               Line5          - Blade input station table
   5.2030E-02   2.6716E-01   1.3308E+01   7.4004E+02   1.5287E+10   1.9789E+10
               Line6          - Blade input station table
   6.8290E-02   2.7941E-01   1.3308E+01   5.9250E+02   1.0782E+10   1.4859E+10
               Line7          - Blade input station table
   8.4550E-02   2.9167E-01   1.3308E+01   4.5027E+02   7.2297E+09   1.0221E+10
               Line8          - Blade input station table
   1.0081E-01   3.0392E-01   1.3308E+01   4.2405E+02   6.3095E+09   9.1447E+09
               Line9          - Blade input station table
   1.1707E-01   3.1618E-01   1.3308E+01   4.0064E+02   5.5284E+09   8.0632E+09
               Line10         - Blade input station table
   1.3335E-01   3.2844E-01   1.3308E+01   3.8206E+02   4.9801E+09   6.8844E+09
               Line11         - Blade input station table
   1.4959E-01   3.4069E-01   1.3308E+01   3.9965E+02   4.9368E+09   7.0092E+09
               Line12         - Blade input station table
   1.6585E-01   3.5294E-01   1.3308E+01   4.2632E+02   4.6917E+09   7.1677E+09
               Line13         - Blade input station table
   1.8211E-01   3.6519E-01   1.3181E+01   4.1682E+02   3.9495E+09   7.2717E+09
               Line14         - Blade input station table
   1.9837E-01   3.7500E-01   1.2848E+01   4.0619E+02   3.3865E+09   7.0817E+09
               Line15         - Blade input station table
   2.1465E-01   3.7500E-01   1.2192E+01   3.8142E+02   2.9337E+09   6.2445E+09
               Line16         - Blade input station table
   2.3089E-01   3.7500E-01   1.1561E+01   3.5282E+02   2.5690E+09   5.0490E+09
               Line17         - Blade input station table
   2.4715E-01   3.7500E-01   1.1072E+01   3.4948E+02   2.3886E+09   4.9485E+09
               Line18         - Blade input station table
   2.6341E-01   3.7500E-01   1.0792E+01   3.4654E+02   2.2720E+09   4.8080E+09
               Line19         - Blade input station table
   2.9595E-01   3.7500E-01   1.0232E+01   3.3933E+02   2.0501E+09   4.5014E+09
               Line20         - Blade input station table
   3.2846E-01   3.7500E-01   9.6720E+00   3.3000E+02   1.8282E+09   4.2441E+09
               Line21         - Blade input station table
   3.6098E-01   3.7500E-01   9.1100E+00   3.2199E+02   1.5887E+09   3.9953E+09
               Line22         - Blade input station table
   3.9350E-01   3.7500E-01   8.5340E+00   3.1382E+02   1.3619E+09   3.7508E+09
               Line23         - Blade input station table
   4.2602E-01   3.7500E-01   7.9320E+00   2.9473E+02   1.1024E+09   3.4471E+09
               Line24         - Blade input station table
   4.5855E-01   3.7500E-01   7.3210E+00   2.8712E+02   8.7580E+08   3.1391E+09
               Line25         - Blade input station table
   4.9106E-01   3.7500E-01   6.7110E+00   2.6334E+02   6.8130E+08   2.7342E+09
               Line26         - Blade input station table
   5.2358E-01   3.7500E-01   6.1220E+00   2.5321E+02   5.3472E+08   2.5549E+09
               Line27         - Blade input station table
   5.5610E-01   3.7500E-01   5.5460E+00   2.4167E+02   4.0890E+08   2.3340E+09
               Line28         - Blade input station table
   5.8862E-01   3.7500E-01   4.9710E+00   2.2064E+02   3.1454E+08   1.8287E+09
               Line29         - Blade input station table
   6.2115E-01   3.7500E-01   4.4010E+00   2.0029E+02   2.3863E+08   1.5841E+09
               Line30         - Blade input station table
   6.5366E-01   3.7500E-01   3.8340E+00   1.7940E+02   1.7588E+08   1.3234E+09
               Line31         - Blade input station table
   6.8618E-01   3.7500E-01   3.3320E+00   1.6509E+02   1.2601E+08   1.1837E+09
               Line32         - Blade input station table
   7.1870E-01   3.7500E-01   2.8900E+00   1.5441E+02   1.0726E+08   1.0202E+09
               Line33         - Blade input station table
   7.5122E-01   3.7500E-01   2.5030E+00   1.3893E+02   9.0880E+07   7.9781E+08
               Line34         - Blade input station table
   7.8376E-01   3.7500E-01   2.1160E+00   1.2955E+02   7.6310E+07   7.0961E+08
               Line35         - Blade input station table
   8.1626E-01   3.7500E-01   1.7300E+00   1.0726E+02   6.1050E+07   5.1819E+08
               Line36         - Blade input station table
   8.4878E-01   3.7500E-01   1.3420E+00   9.8776E+01   4.9480E+07   4.5487E+08
               Line37         - Blade input station table
   8.8130E-01   3.7500E-01   9.5400E-01   9.0248E+01   3.9360E+07   3.9512E+08
               Line38         - Blade input station table
   8.9756E-01   3.7500E-01   7.6000E-01   8.3001E+01   3.4670E+07   3.5372E+08
               Line39         - Blade input station table
   9.1382E-01   3.7500E-01   5.7400E-01   7.2906E+01   3.0410E+07   3.0473E+08
               Line40         - Blade input station table
   9.3008E-01   3.7500E-01   4.0400E-01   6.8772E+01   2.6520E+07   2.8142E+08
               Line41         - Blade input station table
   9.3821E-01   3.7500E-01   3.1900E-01   6.6264E+01   2.3840E+07   2.6171E+08
               Line42         - Blade input station table
   9.4636E-01   3.7500E-01   2.5300E-01   5.9340E+01   1.9630E+07   1.5881E+08
               Line43         - Blade input station table
   9.5447E-01   3.7500E-01   2.1600E-01   5.5914E+01   1.6000E+07   1.3788E+08
               Line44         - Blade input station table
   9.6260E-01   3.7500E-01   1.7800E-01   5.2484E+01   1.2830E+07   1.1879E+08
               Line45         - Blade input station table
   9.7073E-01   3.7500E-01   1.4000E-01   4.9114E+01   1.0080E+07   1.0163E+08
               Line46         - Blade input station table
   9.7886E-01   3.7500E-01   1.0100E-01   4.5818E+01   7.5500E+06   8.5070E+07
               Line47         - Blade input station table
   9.8699E-01   3.7500E-01   6.2000E-02   4.1669E+01   4.6000E+06   6.4260E+07
               Line48         - Blade input station table
   9.9512E-01   3.7500E-01   2.3000E-02   1.1453E+01   2.5000E+05   6.6100E+06
               Line49         - Blade input station table
   1.0000E+00   3.7500E-01   0.0000E+00   1.0319E+01   1.7000E+05   5.0100E+06

   6.2200E-02  BldFl1Sh(1)    - Blade-flap mode-1 shape coefficients
   1.7254E+00  BldFl1Sh(2)    - Blade-flap mode-1 shape coefficients
  -3.2452E+00  BldFl1Sh(3)    - Blade-flap mode-1 shape coefficients
   4.7131E+00  BldFl1Sh(4)    - Blade-flap mode-1 shape coefficients
  -2.2555E+00  BldFl1Sh(5)    - Blade-flap mode-1 shape coefficients
  -5.8090E-01  BldFl2Sh(1)    - Blade-flap mode-2 shape coefficients
   1.2067E+00  BldFl2Sh(2)    - Blade-flap mode-2 shape coefficients
  -1.5535E+01  BldFl2Sh(3)    - Blade-flap mode-2 shape coefficients
   2.9735E+01  BldFl2Sh(4)    - Blade-flap mode-2 shape coefficients
  -1.3825E+01  BldFl2Sh(5)    - Blade-flap mode-2 shape coefficients
   3.6270E-01  BldEdgSh(1)    - Blade-edge mode shape coefficients
   2.5337E+00  BldEdgSh(2)    - Blade-edge mode shape coefficients
  -3.5772E+00  BldEdgSh(3)    - Blade-edge mode shape coefficients
   2.3760E+00  BldEdgSh(4)    - Blade-edge mode shape coefficients
  -6.9520E-01  BldEdgSh(5)    - Blade-edge mode shape coefficients

Tower input data from file "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\t1_ElastoDyn_tower.dat":

           11  NTwInpSt       - Number of tower input stations
   1.0000E+00  TwrFADmp(1)    - Tower fore-aft structural damping ratios (%)
   1.0000E+00  TwrFADmp(2)    - Tower fore-aft structural damping ratios (%)
   1.0000E+00  TwrSSDmp(1)    - Tower side-to-side structural damping ratios (%)
   1.0000E+00  TwrSSDmp(2)    - Tower side-to-side structural damping ratios (%)

   1.0000E+00  FAStTunr(1)    - Tower fore-aft modal stiffness tuners (-)
   1.0000E+00  FAStTunr(2)    - Tower fore-aft modal stiffness tuners (-)
   1.0000E+00  SSStTunr(1)    - Tower side-to-side modal stiffness tuners (-)
   1.0000E+00  SSStTunr(2)    - Tower side-to-side modal stiffness tuners (-)
   1.0000E+00  AdjTwMa        - Factor to adjust tower mass density (-)
   1.0000E+00  AdjFASt        - Factor to adjust tower fore-aft stiffness (-)
   1.0000E+00  AdjSSSt        - Factor to adjust tower side-to-side stiffness (-)

               Line1          - Tower input station table
   0.0000E+00   4.3065E+03   4.7449E+11   4.7449E+11
               Line2          - Tower input station table
   1.0000E-01   4.0304E+03   4.1308E+11   4.1308E+11
               Line3          - Tower input station table
   2.0000E-01   3.7634E+03   3.5783E+11   3.5783E+11
               Line4          - Tower input station table
   3.0000E-01   3.5055E+03   3.0830E+11   3.0830E+11
               Line5          - Tower input station table
   4.0000E-01   3.2567E+03   2.6408E+11   2.6408E+11
               Line6          - Tower input station table
   5.0000E-01   3.0169E+03   2.2480E+11   2.2480E+11
               Line7          - Tower input station table
   6.0000E-01   2.7861E+03   1.9006E+11   1.9006E+11
               Line8          - Tower input station table
   7.0000E-01   2.5645E+03   1.5949E+11   1.5949E+11
               Line9          - Tower input station table
   8.0000E-01   2.3519E+03   1.3277E+11   1.3277E+11
               Line10         - Tower input station table
   9.0000E-01   2.1483E+03   1.0954E+11   1.0954E+11
               Line11         - Tower input station table
   1.0000E+00   1.9539E+03   8.9490E+10   8.9490E+10

   9.8770E-01  TwFAM1Sh(1)    - Tower fore-aft mode-1 shape coefficients (-)
   1.6080E-01  TwFAM1Sh(2)    - Tower fore-aft mode-1 shape coefficients (-)
  -1.8840E-01  TwFAM1Sh(3)    - Tower fore-aft mode-1 shape coefficients (-)
   1.5080E-01  TwFAM1Sh(4)    - Tower fore-aft mode-1 shape coefficients (-)
  -1.1080E-01  TwFAM1Sh(5)    - Tower fore-aft mode-1 shape coefficients (-)
  -1.0297E+00  TwFAM2Sh(1)    - Tower fore-aft mode-2 shape coefficients  (-)
   1.4443E+00  TwFAM2Sh(2)    - Tower fore-aft mode-2 shape coefficients  (-)
   8.8830E-01  TwFAM2Sh(3)    - Tower fore-aft mode-2 shape coefficients  (-)
  -1.2760E-01  TwFAM2Sh(4)    - Tower fore-aft mode-2 shape coefficients  (-)
  -1.7520E-01  TwFAM2Sh(5)    - Tower fore-aft mode-2 shape coefficients  (-)

   9.7920E-01  TwSSM1Sh(1)    - Tower side-to-side mode-1 shape coefficients (-)
   1.6180E-01  TwSSM1Sh(2)    - Tower side-to-side mode-1 shape coefficients (-)
  -1.7970E-01  TwSSM1Sh(3)    - Tower side-to-side mode-1 shape coefficients (-)
   1.4530E-01  TwSSM1Sh(4)    - Tower side-to-side mode-1 shape coefficients (-)
  -1.0650E-01  TwSSM1Sh(5)    - Tower side-to-side mode-1 shape coefficients (-)
  -1.2253E+00  TwSSM2Sh(1)    - Tower side-to-side mode-2 shape coefficients (-)
   1.3297E+00  TwSSM2Sh(2)    - Tower side-to-side mode-2 shape coefficients (-)
   1.0340E+00  TwSSM2Sh(3)    - Tower side-to-side mode-2 shape coefficients (-)
  -1.5080E-01  TwSSM2Sh(4)    - Tower side-to-side mode-2 shape coefficients (-)
   1.2300E-02  TwSSM2Sh(5)    - Tower side-to-side mode-2 shape coefficients (-)
Echo file for AeroDyn 15 primary input file: C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\t1_AeroDyn15.dat
------- AERODYN v15.03.* INPUT FILE ------------------------------------------------                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            
Generated with AeroElasticSE FAST driver                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        
======  General Options  ============================================================================                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           
 True            = Echo                
 default         = DTAero              
 1               = WakeMod             
 2               = AFAeroMod           
 1               = TwrPotent           
 0               = TwrShadow           
 True            = TwrAero             
 False           = FrozenWake          
 False           = CavitCheck          
 False           = Buoyancy            
 False           = CompAA              
 unused          = AA_InputFile        
======  Environmental Conditions  ===================================================================                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           
 default         = AirDens             
 default         = KinVisc             
 default         = SpdSound            
 default         = Patm                
 default         = Pvap                
======  Blade-Element/Momentum Theory Options  ====================================================== [unused when WakeMod=0 or 3]                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              
 2               = SkewMod             
 default         = SkewModFactor       
 True            = TipLoss             
 True            = HubLoss             
 True            = TanInd              
 False           = AIDrag              
 False           = TIDrag              
 Default         = IndToler            
 100             = MaxIter             
======  Dynamic Blade-Element/Momentum Theory Options  ====================================================== [used only when WakeMod=2]                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        
 2               = DBEMT_Mod           
 4.0             = tau1_const          
======  OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options  ================== [used only when WakeMod=3]                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
 t1_OLAF.dat     = OLAFInputFileName   
======  Beddoes-Leishman Unsteady Airfoil Aerodynamics Options  ===================================== [used only when AFAeroMod=2]                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                              
 3               = UAMod               
 True            = FLookup             
======  Airfoil Information =========================================================================                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           
 1               = AFTabMod            
 1               = InCol_Alfa          
 2               = InCol_Cl            
 3               = InCol_Cd            
 4               = InCol_Cm            
 0               = InCol_Cpmin         
 8               = NumAFfiles          
 Airfoils\t1_Aer = AFNames             
 Airfoils\t1_Aer =                     
 Airfoils\t1_Aer =                     
 Airfoils\t1_Aer =                     
 Airfoils\t1_Aer =                     
 Airfoils\t1_Aer =                     
 Airfoils\t1_Aer =                     
 Airfoils\t1_Aer =                     
======  Rotor/Blade Properties  =====================================================================                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           
 True            = UseBlCm             
 t1_AeroDyn15_bl = ADBlFile(1)         
 t1_AeroDyn15_bl = ADBlFile(2)         
 t1_AeroDyn15_bl = ADBlFile(3)         
======  Hub Properties ============================================================================== [used only when Buoyancy=True]                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            
 0.0             = VolHub              
 0.0             = HubCenBx            
======  Nacelle Properties ========================================================================== [used only when Buoyancy=True]                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            
 0.0             = VolNac              
0, 0, 0                NacCenB     - Position of nacelle center of buoyancy from yaw bearing in nacelle coordinates (m)
======  Tail Fin Aerodynamics ========================================================================                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                          
 False           = TFinAero            
 C:\Users\james\ = TFinFile            
======  Tower Influence and Aerodynamics ============================================================ [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True]                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               
 11              = NumTwrNds           
Tower Table Header: TwrElev        TwrDiam        TwrCd          TwrTI          TwrCb                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               
Tower Table Header: (m)              (m)           (-)            (-)            (-)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                
1.000000000000000e+01  6.000000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
1.776000000000000e+01  5.787000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
2.552000000000000e+01  5.574000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
3.328000000000000e+01  5.361000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
4.104000000000000e+01  5.148000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
4.880000000000000e+01  4.935000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
5.656000000000000e+01  4.722000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
6.431999999999999e+01  4.509000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
7.208000000000000e+01  4.296000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
7.984000000000000e+01  4.083000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
8.759999999999999e+01  3.870000000000000e+00  1.000000000000000e+00  1.000000000000000e-01  0.000000000000000e+00
======  Outputs  ====================================================================================                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                           
 True            = SumPrint            
 0               = NBlOuts             
2, 9, 16, 4, 5, 7, 11, 13, 14 BlOutNd     - Blade nodes whose values will be output  (-)
 0               = NTwOuts             
0                      TwOutNd     - Tower nodes whose values will be output  (-)
OutList             - The next line(s) contains a list of output parameters.  See OutListParameters.xlsx for a listing of available output channels, (-)                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                        
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)

           19  NumBlNds       - Number of blade nodes used in the analysis (-)
    BlSpn        BlCrvAC        BlSwpAC        BlCrvAng       BlTwist        BlChord          BlAFID

   0.0000    0.0000    0.0000    0.0000   13.3080    3.5420         1   0.0000    0.0000    0.0000
   1.3667   -0.0008   -0.0034    0.0000   13.3080    3.5420         1   0.0000    0.0000    0.0000
   4.1000   -0.0248   -0.1050    0.0000   13.3080    3.8540         1   0.0000    0.0000    0.0000
   6.8333   -0.0595   -0.2514    0.0000   13.3080    4.1670         2   0.0000    0.0000    0.0000
  10.2500   -0.1091   -0.4612    0.0000   13.3080    4.5570         3   0.0000    0.0000    0.0000
  14.3500   -0.1157   -0.5699    0.0000   11.4800    4.6520         4   0.0000    0.0000    0.0000
  18.4500   -0.0983   -0.5485    0.0000   10.1620    4.4580         4   0.0000    0.0000    0.0000
  22.5500   -0.0832   -0.5246    0.0000    9.0110    4.2490         5   0.0000    0.0000    0.0000
  26.6500   -0.0679   -0.4962    0.0000    7.7950    4.0070         6   0.0000    0.0000    0.0000
  30.7500   -0.0534   -0.4654    0.0000    6.5440    3.7480         6   0.0000    0.0000    0.0000
  34.8500   -0.0409   -0.4358    0.0000    5.3610    3.5020         7   0.0000    0.0000    0.0000
  38.9500   -0.0297   -0.4059    0.0000    4.1880    3.2560         7   0.0000    0.0000    0.0000
  43.0500   -0.0205   -0.3757    0.0000    3.1250    3.0100         8   0.0000    0.0000    0.0000
  47.1500   -0.0140   -0.3452    0.0000    2.3190    2.7640         8   0.0000    0.0000    0.0000
  51.2500   -0.0084   -0.3146    0.0000    1.5260    2.5180         8   0.0000    0.0000    0.0000
  54.6667   -0.0044   -0.2891    0.0000    0.8630    2.3130         8   0.0000    0.0000    0.0000
  57.4000   -0.0017   -0.2607    0.0000    0.3700    2.0860         8   0.0000    0.0000    0.0000
  60.1333   -0.0003   -0.1774    0.0000    0.1060    1.4190         8   0.0000    0.0000    0.0000
  61.4999   -0.0003   -0.1774    0.0000    0.1060    1.4190         8   0.0000    0.0000    0.0000

           19  NumBlNds       - Number of blade nodes used in the analysis (-)
    BlSpn        BlCrvAC        BlSwpAC        BlCrvAng       BlTwist        BlChord          BlAFID

   0.0000    0.0000    0.0000    0.0000   13.3080    3.5420         1   0.0000    0.0000    0.0000
   1.3667   -0.0008   -0.0034    0.0000   13.3080    3.5420         1   0.0000    0.0000    0.0000
   4.1000   -0.0248   -0.1050    0.0000   13.3080    3.8540         1   0.0000    0.0000    0.0000
   6.8333   -0.0595   -0.2514    0.0000   13.3080    4.1670         2   0.0000    0.0000    0.0000
  10.2500   -0.1091   -0.4612    0.0000   13.3080    4.5570         3   0.0000    0.0000    0.0000
  14.3500   -0.1157   -0.5699    0.0000   11.4800    4.6520         4   0.0000    0.0000    0.0000
  18.4500   -0.0983   -0.5485    0.0000   10.1620    4.4580         4   0.0000    0.0000    0.0000
  22.5500   -0.0832   -0.5246    0.0000    9.0110    4.2490         5   0.0000    0.0000    0.0000
  26.6500   -0.0679   -0.4962    0.0000    7.7950    4.0070         6   0.0000    0.0000    0.0000
  30.7500   -0.0534   -0.4654    0.0000    6.5440    3.7480         6   0.0000    0.0000    0.0000
  34.8500   -0.0409   -0.4358    0.0000    5.3610    3.5020         7   0.0000    0.0000    0.0000
  38.9500   -0.0297   -0.4059    0.0000    4.1880    3.2560         7   0.0000    0.0000    0.0000
  43.0500   -0.0205   -0.3757    0.0000    3.1250    3.0100         8   0.0000    0.0000    0.0000
  47.1500   -0.0140   -0.3452    0.0000    2.3190    2.7640         8   0.0000    0.0000    0.0000
  51.2500   -0.0084   -0.3146    0.0000    1.5260    2.5180         8   0.0000    0.0000    0.0000
  54.6667   -0.0044   -0.2891    0.0000    0.8630    2.3130         8   0.0000    0.0000    0.0000
  57.4000   -0.0017   -0.2607    0.0000    0.3700    2.0860         8   0.0000    0.0000    0.0000
  60.1333   -0.0003   -0.1774    0.0000    0.1060    1.4190         8   0.0000    0.0000    0.0000
  61.4999   -0.0003   -0.1774    0.0000    0.1060    1.4190         8   0.0000    0.0000    0.0000

           19  NumBlNds       - Number of blade nodes used in the analysis (-)
    BlSpn        BlCrvAC        BlSwpAC        BlCrvAng       BlTwist        BlChord          BlAFID

   0.0000    0.0000    0.0000    0.0000   13.3080    3.5420         1   0.0000    0.0000    0.0000
   1.3667   -0.0008   -0.0034    0.0000   13.3080    3.5420         1   0.0000    0.0000    0.0000
   4.1000   -0.0248   -0.1050    0.0000   13.3080    3.8540         1   0.0000    0.0000    0.0000
   6.8333   -0.0595   -0.2514    0.0000   13.3080    4.1670         2   0.0000    0.0000    0.0000
  10.2500   -0.1091   -0.4612    0.0000   13.3080    4.5570         3   0.0000    0.0000    0.0000
  14.3500   -0.1157   -0.5699    0.0000   11.4800    4.6520         4   0.0000    0.0000    0.0000
  18.4500   -0.0983   -0.5485    0.0000   10.1620    4.4580         4   0.0000    0.0000    0.0000
  22.5500   -0.0832   -0.5246    0.0000    9.0110    4.2490         5   0.0000    0.0000    0.0000
  26.6500   -0.0679   -0.4962    0.0000    7.7950    4.0070         6   0.0000    0.0000    0.0000
  30.7500   -0.0534   -0.4654    0.0000    6.5440    3.7480         6   0.0000    0.0000    0.0000
  34.8500   -0.0409   -0.4358    0.0000    5.3610    3.5020         7   0.0000    0.0000    0.0000
  38.9500   -0.0297   -0.4059    0.0000    4.1880    3.2560         7   0.0000    0.0000    0.0000
  43.0500   -0.0205   -0.3757    0.0000    3.1250    3.0100         8   0.0000    0.0000    0.0000
  47.1500   -0.0140   -0.3452    0.0000    2.3190    2.7640         8   0.0000    0.0000    0.0000
  51.2500   -0.0084   -0.3146    0.0000    1.5260    2.5180         8   0.0000    0.0000    0.0000
  54.6667   -0.0044   -0.2891    0.0000    0.8630    2.3130         8   0.0000    0.0000    0.0000
  57.4000   -0.0017   -0.2607    0.0000    0.3700    2.0860         8   0.0000    0.0000    0.0000
  60.1333   -0.0003   -0.1774    0.0000    0.1060    1.4190         8   0.0000    0.0000    0.0000
  61.4999   -0.0003   -0.1774    0.0000    0.1060    1.4190         8   0.0000    0.0000    0.0000
--
Contents of "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\Airfoils\t1_AeroDyn15_Polar_00.dat":
 DEFAULT         = InterpOrd           
 1.0             = NonDimArea          
 401             = NumCoords           
0.500000       0
1.00000000000000e+00  0.00000000000000e+00
9.96600000000000e-01  5.82100000000000e-02
9.93140000000000e-01  8.25410000000000e-02
9.89610000000000e-01  1.01400000000000e-01
9.86010000000000e-01  1.17449000000000e-01
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 0.000000        = k1_hat              
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--
Contents of "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\Airfoils\t1_AeroDyn15_Polar_01.dat":
 DEFAULT         = InterpOrd           
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0.416670       0
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1.00000000000000e+00  0.00000000000000e+00
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 AF01_BL.txt     = BL_file             
 1               = NumTabs             
 0.750000        = Re                  
 0               = Ctrl                
 True            = InclUAdata          
 0.000000        = alpha0              
 0.000000        = alpha1              
 0.000000        = alpha2              
 0.000000        = eta_e               
 0.000000        = C_nalpha            
 3.000000        = T_f0                
 3.000000        = T_f0                
 6.000000        = T_V0                
 6.000000        = T_V0                
 1.700000        = T_p                 
 1.700000        = T_p                 
 11.000000       = T_VL                
 11.000000       = T_VL                
 0.140000        = b1                  
 0.140000        = b1                  
 0.530000        = b2                  
 0.530000        = b2                  
 5.000000        = b5                  
 5.000000        = b5                  
 0.300000        = A1                  
 0.300000        = A1                  
 0.700000        = A2                  
 0.700000        = A2                  
 1.000000        = A5                  
 1.000000        = A5                  
 0.000000        = S1                  
 0.000000        = S2                  
 0.000000        = S3                  
 0.000000        = S4                  
 0.000000        = Cn1                 
 0.000000        = Cn2                 
 0.190000        = St_sh               
 0.190000        = St_sh               
 0.350000        = Cd0                 
 0.000000        = Cm0                 
 0.000000        = k0                  
 0.000000        = k1                  
 0.000000        = k2                  
 0.000000        = k3                  
 0.000000        = k1_hat              
 0.200000        = x_cp_bar            
 0.200000        = x_cp_bar            
 DEFAULT         = UACutout            
 DEFAULT         = filtCutOff          
 3               = NumAlf              
-1.80000000000000e+02  0.00000000000000e+00  3.50000000000000e-01  0.00000000000000e+00
0.00000000000000e+00  0.00000000000000e+00  3.50000000000000e-01  0.00000000000000e+00
1.80000000000000e+02  0.00000000000000e+00  3.50000000000000e-01  0.00000000000000e+00
--
Contents of "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\Airfoils\t1_AeroDyn15_Polar_02.dat":
 DEFAULT         = InterpOrd           
 1.0             = NonDimArea          
 401             = NumCoords           
0.330870       0
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 0.750000        = Re                  
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 9.000000        = alpha1              
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 11.000000       = T_VL                
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 1.351900        = Cn1                 
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 0.190000        = St_sh               
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 DEFAULT         = UACutout            
 DEFAULT         = filtCutOff          
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--
Contents of "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\Airfoils\t1_AeroDyn15_Polar_03.dat":
 DEFAULT         = InterpOrd           
 1.0             = NonDimArea          
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0.250000       0
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9.86010000000000e-01  6.83000000000000e-03
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8.42160000000000e-01 -9.96000000000000e-03
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8.53330000000000e-01 -7.27000000000000e-03
8.58820000000000e-01 -6.04000000000000e-03
8.64250000000000e-01 -4.87000000000000e-03
8.69610000000000e-01 -3.77000000000000e-03
8.74900000000000e-01 -2.76000000000000e-03
8.80130000000000e-01 -1.82000000000000e-03
8.85290000000000e-01 -9.50000000000000e-04
8.90390000000000e-01 -1.40000000000000e-04
8.95420000000000e-01  6.10000000000000e-04
9.00390000000000e-01  1.28000000000000e-03
9.05290000000000e-01  1.89000000000000e-03
9.10130000000000e-01  2.43000000000000e-03
9.14900000000000e-01  2.93000000000000e-03
9.19610000000000e-01  3.35000000000000e-03
9.24250000000000e-01  3.70000000000000e-03
9.28820000000000e-01  4.01000000000000e-03
9.33330000000000e-01  4.25000000000000e-03
9.37780000000000e-01  4.41000000000000e-03
9.42160000000000e-01  4.52000000000000e-03
9.46470000000000e-01  4.55000000000000e-03
9.50720000000000e-01  4.51000000000000e-03
9.54900000000000e-01  4.39000000000000e-03
9.59020000000000e-01  4.20000000000000e-03
9.63070000000000e-01  3.94000000000000e-03
9.67060000000000e-01  3.58000000000000e-03
9.70980000000000e-01  3.15000000000000e-03
9.74840000000000e-01  2.64000000000000e-03
9.78630000000000e-01  2.06000000000000e-03
9.82350000000000e-01  1.41000000000000e-03
9.86010000000000e-01  6.90000000000000e-04
9.89610000000000e-01 -1.10000000000000e-04
9.93140000000000e-01 -9.70000000000000e-04
9.96600000000000e-01 -1.90000000000000e-03
1.00000000000000e+00 -2.83000000000000e-03
0.00000000000000e+00  0.00000000000000e+00
James-Ilosta commented 9 months ago 
AF03_BL.txt     = BL_file             
 1               = NumTabs             
 0.750000        = Re                  
 0               = Ctrl                
 True            = InclUAdata          
 -1.200000       = alpha0              
 11.500000       = alpha1              
 -11.500000      = alpha2              
 1.000000        = eta_e               
 7.183800        = C_nalpha            
 3.000000        = T_f0                
 3.000000        = T_f0                
 6.000000        = T_V0                
 6.000000        = T_V0                
 1.700000        = T_p                 
 1.700000        = T_p                 
 11.000000       = T_VL                
 11.000000       = T_VL                
 0.140000        = b1                  
 0.140000        = b1                  
 0.530000        = b2                  
 0.530000        = b2                  
 5.000000        = b5                  
 5.000000        = b5                  
 0.300000        = A1                  
 0.300000        = A1                  
 0.700000        = A2                  
 0.700000        = A2                  
 1.000000        = A5                  
 1.000000        = A5                  
 0.000000        = S1                  
 0.000000        = S2                  
 0.000000        = S3                  
 0.000000        = S4                  
 1.671700        = Cn1                 
 -0.307500       = Cn2                 
 0.190000        = St_sh               
 0.190000        = St_sh               
 0.012000        = Cd0                 
 -0.070000       = Cm0                 
 0.000000        = k0                  
 0.000000        = k1                  
 0.000000        = k2                  
 0.000000        = k3                  
 0.000000        = k1_hat              
 0.200000        = x_cp_bar            
 0.200000        = x_cp_bar            
 DEFAULT         = UACutout            
 DEFAULT         = filtCutOff          
 135             = NumAlf              
-1.80000000000000e+02  0.00000000000000e+00  4.07000000000000e-02  0.00000000000000e+00
-1.75000000000000e+02  2.23000000000000e-01  5.07000000000000e-02  9.37000000000000e-02
-1.70000000000000e+02  4.05000000000000e-01  1.05500000000000e-01  1.70200000000000e-01
-1.60000000000000e+02  6.58000000000000e-01  2.98200000000000e-01  2.81900000000000e-01
-1.55000000000000e+02  7.33000000000000e-01  4.12100000000000e-01  3.21300000000000e-01
-1.50000000000000e+02  7.78000000000000e-01  5.30800000000000e-01  3.52000000000000e-01
-1.45000000000000e+02  7.95000000000000e-01  6.50300000000000e-01  3.75400000000000e-01
-1.40000000000000e+02  7.87000000000000e-01  7.67200000000000e-01  3.92600000000000e-01
-1.35000000000000e+02  7.57000000000000e-01  8.78500000000000e-01  4.04600000000000e-01
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--
Contents of "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\Airfoils\t1_AeroDyn15_Polar_04.dat":
 DEFAULT         = InterpOrd           
 1.0             = NonDimArea          
 401             = NumCoords           
0.250000       0
1.00000000000000e+00  2.46000000000000e-03
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1.88160000000000e-01  1.21970000000000e-01
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1.65870000000000e-01  1.16440000000000e-01
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1.55260000000000e-01  1.13420000000000e-01
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1.20870000000000e-01  1.01720000000000e-01
1.16310000000000e-01  9.99300000000000e-02
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1.07450000000000e-01  9.62700000000000e-02
1.03150000000000e-01  9.44100000000000e-02
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 AF04_BL.txt     = BL_file             
 1               = NumTabs             
 0.750000        = Re                  
 0               = Ctrl                
 True            = InclUAdata          
 -2.200000       = alpha0              
 9.000000        = alpha1              
 -9.000000       = alpha2              
 1.000000        = eta_e               
 7.332600        = C_nalpha            
 3.000000        = T_f0                
 3.000000        = T_f0                
 6.000000        = T_V0                
 6.000000        = T_V0                
 1.700000        = T_p                 
 1.700000        = T_p                 
 11.000000       = T_VL                
 11.000000       = T_VL                
 0.140000        = b1                  
 0.140000        = b1                  
 0.530000        = b2                  
 0.530000        = b2                  
 5.000000        = b5                  
 5.000000        = b5                  
 0.300000        = A1                  
 0.300000        = A1                  
 0.700000        = A2                  
 0.700000        = A2                  
 1.000000        = A5                  
 1.000000        = A5                  
 0.000000        = S1                  
 0.000000        = S2                  
 0.000000        = S3                  
 0.000000        = S4                  
 1.449000        = Cn1                 
 -0.613800       = Cn2                 
 0.190000        = St_sh               
 0.190000        = St_sh               
 0.008000        = Cd0                 
 -0.090000       = Cm0                 
 0.000000        = k0                  
 0.000000        = k1                  
 0.000000        = k2                  
 0.000000        = k3                  
 0.000000        = k1_hat              
 0.200000        = x_cp_bar            
 0.200000        = x_cp_bar            
 DEFAULT         = UACutout            
 DEFAULT         = filtCutOff          
 143             = NumAlf              
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6.50000000000000e+00  1.13500000000000e+00  1.03000000000000e-02 -1.28000000000000e-01
7.00000000000000e+00  1.19700000000000e+00  1.07000000000000e-02 -1.28700000000000e-01
7.50000000000000e+00  1.25600000000000e+00  1.12000000000000e-02 -1.28900000000000e-01
8.00000000000000e+00  1.30500000000000e+00  1.25000000000000e-02 -1.27000000000000e-01
9.00000000000000e+00  1.39000000000000e+00  1.55000000000000e-02 -1.20700000000000e-01
9.50000000000000e+00  1.42400000000000e+00  1.71000000000000e-02 -1.15800000000000e-01
1.00000000000000e+01  1.45800000000000e+00  1.92000000000000e-02 -1.11600000000000e-01
1.05000000000000e+01  1.48800000000000e+00  2.19000000000000e-02 -1.07300000000000e-01
1.10000000000000e+01  1.51200000000000e+00  2.55000000000000e-02 -1.02900000000000e-01
1.15000000000000e+01  1.53300000000000e+00  3.07000000000000e-02 -9.83000000000000e-02
1.20000000000000e+01  1.54900000000000e+00  3.70000000000000e-02 -9.49000000000000e-02
1.25000000000000e+01  1.55800000000000e+00  4.52000000000000e-02 -9.21000000000000e-02
1.30000000000000e+01  1.47000000000000e+00  6.30000000000000e-02 -8.99000000000000e-02
1.35000000000000e+01  1.39800000000000e+00  7.84000000000000e-02 -8.85000000000000e-02
1.40000000000000e+01  1.35400000000000e+00  9.31000000000000e-02 -8.85000000000000e-02
1.45000000000000e+01  1.33600000000000e+00  1.08100000000000e-01 -9.02000000000000e-02
1.50000000000000e+01  1.33300000000000e+00  1.23900000000000e-01 -9.28000000000000e-02
1.55000000000000e+01  1.32600000000000e+00  1.41500000000000e-01 -9.63000000000000e-02
1.60000000000000e+01  1.32900000000000e+00  1.59200000000000e-01 -1.00600000000000e-01
1.65000000000000e+01  1.32600000000000e+00  1.74300000000000e-01 -1.04200000000000e-01
1.70000000000000e+01  1.32100000000000e+00  1.90300000000000e-01 -1.08400000000000e-01
1.75000000000000e+01  1.33100000000000e+00  2.04400000000000e-01 -1.12500000000000e-01
1.80000000000000e+01  1.33300000000000e+00  2.18600000000000e-01 -1.16900000000000e-01
1.85000000000000e+01  1.34000000000000e+00  2.32400000000000e-01 -1.21500000000000e-01
1.90000000000000e+01  1.36200000000000e+00  2.45500000000000e-01 -1.26300000000000e-01
1.95000000000000e+01  1.38200000000000e+00  2.58400000000000e-01 -1.31300000000000e-01
2.00000000000000e+01  1.39800000000000e+00  2.68900000000000e-01 -1.35200000000000e-01
2.05000000000000e+01  1.42600000000000e+00  2.81400000000000e-01 -1.40600000000000e-01
2.10000000000000e+01  1.43700000000000e+00  2.94300000000000e-01 -1.46200000000000e-01
2.20000000000000e+01  1.41800000000000e+00  3.24600000000000e-01 -1.51600000000000e-01
2.30000000000000e+01  1.39700000000000e+00  3.55700000000000e-01 -1.57000000000000e-01
2.40000000000000e+01  1.37600000000000e+00  3.87500000000000e-01 -1.62300000000000e-01
2.50000000000000e+01  1.35400000000000e+00  4.19800000000000e-01 -1.67600000000000e-01
2.60000000000000e+01  1.33200000000000e+00  4.52400000000000e-01 -1.72800000000000e-01
2.80000000000000e+01  1.29300000000000e+00  5.18300000000000e-01 -1.83200000000000e-01
3.00000000000000e+01  1.26500000000000e+00  5.84300000000000e-01 -1.93500000000000e-01
3.20000000000000e+01  1.25300000000000e+00  6.49200000000000e-01 -2.03900000000000e-01
3.50000000000000e+01  1.26400000000000e+00  7.43800000000000e-01 -2.19300000000000e-01
4.00000000000000e+01  1.25800000000000e+00  8.97000000000000e-01 -2.44000000000000e-01
4.50000000000000e+01  1.21700000000000e+00  1.04020000000000e+00 -2.67200000000000e-01
5.00000000000000e+01  1.14600000000000e+00  1.16860000000000e+00 -2.89100000000000e-01
5.50000000000000e+01  1.04900000000000e+00  1.27790000000000e+00 -3.09700000000000e-01
6.00000000000000e+01  9.32000000000000e-01  1.36470000000000e+00 -3.29000000000000e-01
6.50000000000000e+01  7.99000000000000e-01  1.42670000000000e+00 -3.47100000000000e-01
7.00000000000000e+01  6.57000000000000e-01  1.46210000000000e+00 -3.64100000000000e-01
7.50000000000000e+01  5.09000000000000e-01  1.47080000000000e+00 -3.79900000000000e-01
8.00000000000000e+01  3.62000000000000e-01  1.45440000000000e+00 -3.94600000000000e-01
8.50000000000000e+01  2.21000000000000e-01  1.41960000000000e+00 -4.08100000000000e-01
9.00000000000000e+01  9.20000000000000e-02  1.39380000000000e+00 -4.20400000000000e-01
9.50000000000000e+01 -3.00000000000000e-02  1.39430000000000e+00 -4.31300000000000e-01
1.00000000000000e+02 -1.50000000000000e-01  1.37980000000000e+00 -4.40800000000000e-01
1.05000000000000e+02 -2.67000000000000e-01  1.35040000000000e+00 -4.48600000000000e-01
1.10000000000000e+02 -3.79000000000000e-01  1.30630000000000e+00 -4.54600000000000e-01
1.15000000000000e+02 -4.83000000000000e-01  1.24810000000000e+00 -4.58400000000000e-01
1.20000000000000e+02 -5.78000000000000e-01  1.17630000000000e+00 -4.59700000000000e-01
1.25000000000000e+02 -6.60000000000000e-01  1.09190000000000e+00 -4.58200000000000e-01
1.30000000000000e+02 -7.27000000000000e-01  9.96200000000000e-01 -4.53200000000000e-01
1.35000000000000e+02 -7.77000000000000e-01  8.90600000000000e-01 -4.44100000000000e-01
1.40000000000000e+02 -8.07000000000000e-01  7.77100000000000e-01 -4.30300000000000e-01
1.45000000000000e+02 -8.15000000000000e-01  6.58100000000000e-01 -4.10900000000000e-01
1.50000000000000e+02 -7.97000000000000e-01  5.36400000000000e-01 -3.84800000000000e-01
1.55000000000000e+02 -7.50000000000000e-01  4.15700000000000e-01 -3.50800000000000e-01
1.60000000000000e+02 -6.73000000000000e-01  3.00000000000000e-01 -3.07400000000000e-01
1.70000000000000e+02 -5.47000000000000e-01  1.05100000000000e-01 -2.78600000000000e-01
1.75000000000000e+02 -2.74000000000000e-01  3.88000000000000e-02 -1.38000000000000e-01
1.80000000000000e+02  0.00000000000000e+00  2.67000000000000e-02  0.00000000000000e+00
--
Contents of "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\Airfoils\t1_AeroDyn15_Polar_05.dat":
 DEFAULT         = InterpOrd           
 1.0             = NonDimArea          
 401             = NumCoords           
0.250000       0
1.00000000000000e+00  2.13000000000000e-03
9.96600000000000e-01  3.14000000000000e-03
9.93140000000000e-01  4.14000000000000e-03
9.89610000000000e-01  5.15000000000000e-03
9.86010000000000e-01  6.17000000000000e-03
9.82350000000000e-01  7.20000000000000e-03
9.78630000000000e-01  8.22000000000000e-03
9.74840000000000e-01  9.26000000000000e-03
9.70980000000000e-01  1.03000000000000e-02
9.67060000000000e-01  1.13500000000000e-02
9.63070000000000e-01  1.24000000000000e-02
9.59020000000000e-01  1.34700000000000e-02
9.54900000000000e-01  1.45400000000000e-02
9.50720000000000e-01  1.56200000000000e-02
9.46470000000000e-01  1.67200000000000e-02
9.42160000000000e-01  1.78300000000000e-02
9.37780000000000e-01  1.89500000000000e-02
9.33330000000000e-01  2.00900000000000e-02
9.28820000000000e-01  2.12500000000000e-02
9.24250000000000e-01  2.24100000000000e-02
9.19610000000000e-01  2.35900000000000e-02
9.14900000000000e-01  2.47900000000000e-02
9.10130000000000e-01  2.60000000000000e-02
9.05290000000000e-01  2.72200000000000e-02
9.00390000000000e-01  2.84600000000000e-02
8.95420000000000e-01  2.97200000000000e-02
8.90390000000000e-01  3.09900000000000e-02
8.85290000000000e-01  3.22700000000000e-02
8.80130000000000e-01  3.35700000000000e-02
8.74900000000000e-01  3.48900000000000e-02
8.69610000000000e-01  3.62200000000000e-02
8.64250000000000e-01  3.75600000000000e-02
8.58820000000000e-01  3.89200000000000e-02
8.53330000000000e-01  4.02900000000000e-02
8.47780000000000e-01  4.16700000000000e-02
8.42160000000000e-01  4.30600000000000e-02
8.36470000000000e-01  4.44700000000000e-02
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8.24900000000000e-01  4.73200000000000e-02
8.19020000000000e-01  4.87700000000000e-02
8.13070000000000e-01  5.02300000000000e-02
8.07060000000000e-01  5.17000000000000e-02
8.00980000000000e-01  5.31900000000000e-02
7.94840000000000e-01  5.46800000000000e-02
7.88630000000000e-01  5.61900000000000e-02
7.82350000000000e-01  5.77100000000000e-02
7.76010000000000e-01  5.92500000000000e-02
7.69610000000000e-01  6.07800000000000e-02
7.63140000000000e-01  6.23300000000000e-02
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7.50000000000000e-01  6.54400000000000e-02
7.43330000000000e-01  6.70100000000000e-02
7.36670000000000e-01  6.85700000000000e-02
7.30000000000000e-01  7.01300000000000e-02
7.23330000000000e-01  7.16800000000000e-02
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7.10000000000000e-01  7.47500000000000e-02
7.03330000000000e-01  7.62800000000000e-02
6.96670000000000e-01  7.77900000000000e-02
6.90000000000000e-01  7.93000000000000e-02
6.83330000000000e-01  8.08000000000000e-02
6.76670000000000e-01  8.22800000000000e-02
6.70000000000000e-01  8.37500000000000e-02
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6.56670000000000e-01  8.66700000000000e-02
6.50000000000000e-01  8.81000000000000e-02
6.43330000000000e-01  8.95300000000000e-02
6.36670000000000e-01  9.09300000000000e-02
6.30000000000000e-01  9.23300000000000e-02
6.23330000000000e-01  9.37100000000000e-02
6.16670000000000e-01  9.50700000000000e-02
6.10000000000000e-01  9.64200000000000e-02
6.03330000000000e-01  9.77500000000000e-02
5.96670000000000e-01  9.90600000000000e-02
5.90000000000000e-01  1.00350000000000e-01
5.83330000000000e-01  1.01630000000000e-01
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5.63330000000000e-01  1.05350000000000e-01
5.56670000000000e-01  1.06550000000000e-01
5.50000000000000e-01  1.07730000000000e-01
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5.36670000000000e-01  1.10010000000000e-01
5.30000000000000e-01  1.11120000000000e-01
5.23330000000000e-01  1.12210000000000e-01
5.16670000000000e-01  1.13270000000000e-01
5.10000000000000e-01  1.14300000000000e-01
5.03330000000000e-01  1.15300000000000e-01
4.96670000000000e-01  1.16280000000000e-01
4.90000000000000e-01  1.17230000000000e-01
4.83330000000000e-01  1.18150000000000e-01
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4.70000000000000e-01  1.19910000000000e-01
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4.56670000000000e-01  1.21540000000000e-01
4.50000000000000e-01  1.22300000000000e-01
4.43330000000000e-01  1.23030000000000e-01
4.36670000000000e-01  1.23720000000000e-01
4.30000000000000e-01  1.24360000000000e-01
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3.90000000000000e-01  1.27380000000000e-01
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3.56670000000000e-01  1.28580000000000e-01
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2.83330000000000e-01  1.25380000000000e-01
2.76670000000000e-01  1.24690000000000e-01
2.70000000000000e-01  1.23940000000000e-01
2.63330000000000e-01  1.23120000000000e-01
2.56670000000000e-01  1.22240000000000e-01
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2.43420000000000e-01  1.20300000000000e-01
2.36930000000000e-01  1.19260000000000e-01
2.30530000000000e-01  1.18170000000000e-01
2.24210000000000e-01  1.17040000000000e-01
2.17980000000000e-01  1.15860000000000e-01
2.11840000000000e-01  1.14650000000000e-01
2.05790000000000e-01  1.13400000000000e-01
1.99820000000000e-01  1.12100000000000e-01
1.93950000000000e-01  1.10780000000000e-01
1.88160000000000e-01  1.09420000000000e-01
1.82450000000000e-01  1.08030000000000e-01
1.76840000000000e-01  1.06600000000000e-01
1.71310000000000e-01  1.05150000000000e-01
1.65870000000000e-01  1.03670000000000e-01
1.60520000000000e-01  1.02170000000000e-01
1.55260000000000e-01  1.00640000000000e-01
1.50080000000000e-01  9.90900000000000e-02
1.44990000000000e-01  9.75100000000000e-02
1.39990000000000e-01  9.59100000000000e-02
1.35080000000000e-01  9.43000000000000e-02
1.30260000000000e-01  9.26600000000000e-02
1.25520000000000e-01  9.10100000000000e-02
1.20870000000000e-01  8.93400000000000e-02
1.16310000000000e-01  8.76500000000000e-02
1.11830000000000e-01  8.59500000000000e-02
1.07450000000000e-01  8.42400000000000e-02
1.03150000000000e-01  8.25100000000000e-02
9.89300000000000e-02  8.07600000000000e-02
9.48100000000000e-02  7.90200000000000e-02
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8.68300000000000e-02  7.54900000000000e-02
8.29700000000000e-02  7.37100000000000e-02
7.91900000000000e-02  7.19200000000000e-02
7.55100000000000e-02  7.01300000000000e-02
7.19100000000000e-02  6.83400000000000e-02
6.84000000000000e-02  6.65400000000000e-02
6.49800000000000e-02  6.47400000000000e-02
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5.84000000000000e-02  6.11300000000000e-02
5.52400000000000e-02  5.93300000000000e-02
5.21700000000000e-02  5.75300000000000e-02
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3.81200000000000e-02  4.85600000000000e-02
3.55800000000000e-02  4.67900000000000e-02
3.31200000000000e-02  4.50200000000000e-02
3.07500000000000e-02  4.32600000000000e-02
2.84700000000000e-02  4.15100000000000e-02
2.62700000000000e-02  3.97600000000000e-02
2.41700000000000e-02  3.80400000000000e-02
2.21500000000000e-02  3.63200000000000e-02
2.02200000000000e-02  3.46200000000000e-02
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1.66200000000000e-02  3.12600000000000e-02
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1.18700000000000e-02  2.63500000000000e-02
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4.76000000000000e-03  1.70600000000000e-02
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1.24000000000000e-03  9.45000000000000e-03
8.00000000000000e-04  7.66000000000000e-03
4.40000000000000e-04  5.68000000000000e-03
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0.00000000000000e+00  0.00000000000000e+00
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1.24000000000000e-03 -9.74000000000000e-03
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2.38000000000000e-03 -1.35900000000000e-02
3.09000000000000e-03 -1.54900000000000e-02
3.88000000000000e-03 -1.73600000000000e-02
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5.72000000000000e-03 -2.10400000000000e-02
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7.92000000000000e-03 -2.47000000000000e-02
9.15000000000000e-03 -2.65200000000000e-02
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1.49500000000000e-02 -3.39200000000000e-02
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1.83700000000000e-02 -3.77000000000000e-02
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3.16670000000000e-01 -1.22070000000000e-01
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3.96670000000000e-01 -1.15370000000000e-01
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6.03330000000000e-01 -6.18000000000000e-02
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6.30000000000000e-01 -5.24200000000000e-02
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6.43330000000000e-01 -4.76700000000000e-02
6.50000000000000e-01 -4.53000000000000e-02
6.56670000000000e-01 -4.29300000000000e-02
6.63330000000000e-01 -4.05700000000000e-02
6.70000000000000e-01 -3.82200000000000e-02
6.76670000000000e-01 -3.58800000000000e-02
6.83330000000000e-01 -3.35700000000000e-02
6.90000000000000e-01 -3.12700000000000e-02
6.96670000000000e-01 -2.90000000000000e-02
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7.10000000000000e-01 -2.45600000000000e-02
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7.30000000000000e-01 -1.81700000000000e-02
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7.43330000000000e-01 -1.41600000000000e-02
7.50000000000000e-01 -1.22300000000000e-02
7.56600000000000e-01 -1.03800000000000e-02
7.63140000000000e-01 -8.61000000000000e-03
7.69610000000000e-01 -6.92000000000000e-03
7.76010000000000e-01 -5.32000000000000e-03
7.82350000000000e-01 -3.81000000000000e-03
7.88630000000000e-01 -2.38000000000000e-03
7.94840000000000e-01 -1.03000000000000e-03
8.00980000000000e-01  2.30000000000000e-04
8.07060000000000e-01  1.41000000000000e-03
8.13070000000000e-01  2.50000000000000e-03
8.19020000000000e-01  3.51000000000000e-03
8.24900000000000e-01  4.44000000000000e-03
8.30720000000000e-01  5.29000000000000e-03
8.36470000000000e-01  6.06000000000000e-03
8.42160000000000e-01  6.75000000000000e-03
8.47780000000000e-01  7.37000000000000e-03
8.53330000000000e-01  7.91000000000000e-03
8.58820000000000e-01  8.39000000000000e-03
8.64250000000000e-01  8.79000000000000e-03
8.69610000000000e-01  9.13000000000000e-03
8.74900000000000e-01  9.40000000000000e-03
8.80130000000000e-01  9.61000000000000e-03
8.85290000000000e-01  9.75000000000000e-03
8.90390000000000e-01  9.83000000000000e-03
8.95420000000000e-01  9.85000000000000e-03
9.00390000000000e-01  9.82000000000000e-03
9.05290000000000e-01  9.72000000000000e-03
9.10130000000000e-01  9.57000000000000e-03
9.14900000000000e-01  9.36000000000000e-03
9.19610000000000e-01  9.10000000000000e-03
9.24250000000000e-01  8.80000000000000e-03
9.28820000000000e-01  8.44000000000000e-03
9.33330000000000e-01  8.04000000000000e-03
9.37780000000000e-01  7.60000000000000e-03
9.42160000000000e-01  7.12000000000000e-03
9.46470000000000e-01  6.60000000000000e-03
9.50720000000000e-01  6.06000000000000e-03
9.54900000000000e-01  5.49000000000000e-03
9.59020000000000e-01  4.90000000000000e-03
9.63070000000000e-01  4.29000000000000e-03
9.67060000000000e-01  3.67000000000000e-03
9.70980000000000e-01  3.03000000000000e-03
9.74840000000000e-01  2.38000000000000e-03
9.78630000000000e-01  1.73000000000000e-03
9.82350000000000e-01  1.08000000000000e-03
9.86010000000000e-01  4.30000000000000e-04
9.89610000000000e-01 -2.20000000000000e-04
9.93140000000000e-01 -8.60000000000000e-04
9.96600000000000e-01 -1.49000000000000e-03
1.00000000000000e+00 -2.13000000000000e-03
0.00000000000000e+00  0.00000000000000e+00
 AF05_BL.txt     = BL_file             
 1               = NumTabs             
 0.750000        = Re                  
 0               = Ctrl                
 True            = InclUAdata          
 -3.200000       = alpha0              
 8.500000        = alpha1              
 -8.500000       = alpha2              
 1.000000        = eta_e               
 6.446200        = C_nalpha            
 3.000000        = T_f0                
 3.000000        = T_f0                
 6.000000        = T_V0                
 6.000000        = T_V0                
 1.700000        = T_p                 
 1.700000        = T_p                 
 11.000000       = T_VL                
 11.000000       = T_VL                
 0.140000        = b1                  
 0.140000        = b1                  
 0.530000        = b2                  
 0.530000        = b2                  
 5.000000        = b5                  
 5.000000        = b5                  
 0.300000        = A1                  
 0.300000        = A1                  
 0.700000        = A2                  
 0.700000        = A2                  
 1.000000        = A5                  
 1.000000        = A5                  
 0.000000        = S1                  
 0.000000        = S2                  
 0.000000        = S3                  
 0.000000        = S4                  
 1.433600        = Cn1                 
 -0.687300       = Cn2                 
 0.190000        = St_sh               
 0.190000        = St_sh               
 0.006000        = Cd0                 
 -0.120000       = Cm0                 
 0.000000        = k0                  
 0.000000        = k1                  
 0.000000        = k2                  
 0.000000        = k3                  
 0.000000        = k1_hat              
 0.200000        = x_cp_bar            
 0.200000        = x_cp_bar            
 DEFAULT         = UACutout            
 DEFAULT         = filtCutOff          
 140             = NumAlf              
-1.80000000000000e+02  0.00000000000000e+00  2.02000000000000e-02  0.00000000000000e+00
-1.75000000000000e+02  3.68000000000000e-01  3.24000000000000e-02  1.84500000000000e-01
-1.70000000000000e+02  7.35000000000000e-01  9.43000000000000e-02  3.70100000000000e-01
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-1.35000000000000e+02  8.18000000000000e-01  8.82300000000000e-01  3.79400000000000e-01
-1.30000000000000e+02  7.71000000000000e-01  9.91100000000000e-01  3.85400000000000e-01
-1.25000000000000e+02  7.05000000000000e-01  1.09050000000000e+00  3.87800000000000e-01
-1.20000000000000e+02  6.24000000000000e-01  1.17870000000000e+00  3.87200000000000e-01
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-9.50000000000000e+01  7.30000000000000e-02  1.41690000000000e+00  3.52900000000000e-01
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5.00000000000000e-01  5.08000000000000e-01  6.50000000000000e-03 -1.34700000000000e-01
1.00000000000000e+00  5.73000000000000e-01  6.60000000000000e-03 -1.36400000000000e-01
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1.05000000000000e+01  1.42700000000000e+00  3.36000000000000e-02 -1.11500000000000e-01
1.10000000000000e+01  1.37400000000000e+00  4.20000000000000e-02 -1.08100000000000e-01
1.15000000000000e+01  1.31600000000000e+00  5.15000000000000e-02 -1.05200000000000e-01
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1.50000000000000e+02 -8.06000000000000e-01  5.26400000000000e-01 -3.83600000000000e-01
1.55000000000000e+02 -7.58000000000000e-01  4.06000000000000e-01 -3.49700000000000e-01
1.60000000000000e+02 -6.79000000000000e-01  2.91200000000000e-01 -3.06500000000000e-01
1.70000000000000e+02 -7.35000000000000e-01  9.95000000000000e-02 -3.70600000000000e-01
1.75000000000000e+02 -3.68000000000000e-01  3.56000000000000e-02 -1.84600000000000e-01
1.80000000000000e+02  0.00000000000000e+00  2.02000000000000e-02  0.00000000000000e+00
--
Contents of "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\Airfoils\t1_AeroDyn15_Polar_06.dat":
 DEFAULT         = InterpOrd           
 1.0             = NonDimArea          
 401             = NumCoords           
0.250000       0
1.00000000000000e+00  1.94000000000000e-03
9.96600000000000e-01  3.04000000000000e-03
9.93140000000000e-01  4.11000000000000e-03
9.89610000000000e-01  5.16000000000000e-03
9.86010000000000e-01  6.18000000000000e-03
9.82350000000000e-01  7.20000000000000e-03
9.78630000000000e-01  8.23000000000000e-03
9.74840000000000e-01  9.27000000000000e-03
9.70980000000000e-01  1.03300000000000e-02
9.67060000000000e-01  1.13900000000000e-02
9.63070000000000e-01  1.24600000000000e-02
9.59020000000000e-01  1.35400000000000e-02
9.54900000000000e-01  1.46300000000000e-02
9.50720000000000e-01  1.57300000000000e-02
9.46470000000000e-01  1.68400000000000e-02
9.42160000000000e-01  1.79700000000000e-02
9.37780000000000e-01  1.91100000000000e-02
9.33330000000000e-01  2.02600000000000e-02
9.28820000000000e-01  2.14200000000000e-02
9.24250000000000e-01  2.26000000000000e-02
9.19610000000000e-01  2.37900000000000e-02
9.14900000000000e-01  2.49900000000000e-02
9.10130000000000e-01  2.62100000000000e-02
9.05290000000000e-01  2.74400000000000e-02
9.00390000000000e-01  2.86900000000000e-02
8.95420000000000e-01  2.99500000000000e-02
8.90390000000000e-01  3.12200000000000e-02
8.85290000000000e-01  3.25000000000000e-02
8.80130000000000e-01  3.37900000000000e-02
8.74900000000000e-01  3.51000000000000e-02
8.69610000000000e-01  3.64300000000000e-02
8.64250000000000e-01  3.77600000000000e-02
8.58820000000000e-01  3.91200000000000e-02
8.53330000000000e-01  4.04800000000000e-02
8.47780000000000e-01  4.18600000000000e-02
8.42160000000000e-01  4.32600000000000e-02
8.36470000000000e-01  4.46600000000000e-02
8.30720000000000e-01  4.60800000000000e-02
8.24900000000000e-01  4.75200000000000e-02
8.19020000000000e-01  4.89600000000000e-02
8.13070000000000e-01  5.04100000000000e-02
8.07060000000000e-01  5.18800000000000e-02
8.00980000000000e-01  5.33600000000000e-02
7.94840000000000e-01  5.48400000000000e-02
7.88630000000000e-01  5.63400000000000e-02
7.82350000000000e-01  5.78400000000000e-02
7.76010000000000e-01  5.93600000000000e-02
7.69610000000000e-01  6.08800000000000e-02
7.63140000000000e-01  6.24200000000000e-02
7.56600000000000e-01  6.39600000000000e-02
7.50000000000000e-01  6.55000000000000e-02
7.43330000000000e-01  6.70600000000000e-02
7.36670000000000e-01  6.86000000000000e-02
7.30000000000000e-01  7.01400000000000e-02
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7.10000000000000e-01  7.47200000000000e-02
7.03330000000000e-01  7.62400000000000e-02
6.96670000000000e-01  7.77400000000000e-02
6.90000000000000e-01  7.92400000000000e-02
6.83330000000000e-01  8.07200000000000e-02
6.76670000000000e-01  8.22000000000000e-02
6.70000000000000e-01  8.36600000000000e-02
6.63330000000000e-01  8.51100000000000e-02
6.56670000000000e-01  8.65500000000000e-02
6.50000000000000e-01  8.79800000000000e-02
6.43330000000000e-01  8.94000000000000e-02
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6.30000000000000e-01  9.22000000000000e-02
6.23330000000000e-01  9.35700000000000e-02
6.16670000000000e-01  9.49200000000000e-02
6.10000000000000e-01  9.62600000000000e-02
6.03330000000000e-01  9.75900000000000e-02
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5.90000000000000e-01  1.00170000000000e-01
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5.63330000000000e-01  1.05090000000000e-01
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2.56670000000000e-01  1.16530000000000e-01
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2.17980000000000e-01  1.10150000000000e-01
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2.05790000000000e-01  1.07730000000000e-01
1.99820000000000e-01  1.06480000000000e-01
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1.88160000000000e-01  1.03890000000000e-01
1.82450000000000e-01  1.02550000000000e-01
1.76840000000000e-01  1.01190000000000e-01
1.71310000000000e-01  9.98000000000000e-02
1.65870000000000e-01  9.83900000000000e-02
1.60520000000000e-01  9.69600000000000e-02
1.55260000000000e-01  9.55000000000000e-02
1.50080000000000e-01  9.40300000000000e-02
1.44990000000000e-01  9.25400000000000e-02
1.39990000000000e-01  9.10300000000000e-02
1.35080000000000e-01  8.95000000000000e-02
1.30260000000000e-01  8.79600000000000e-02
1.25520000000000e-01  8.64100000000000e-02
1.20870000000000e-01  8.48300000000000e-02
1.16310000000000e-01  8.32500000000000e-02
1.11830000000000e-01  8.16500000000000e-02
1.07450000000000e-01  8.00400000000000e-02
1.03150000000000e-01  7.84300000000000e-02
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8.68300000000000e-02  7.18600000000000e-02
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 3.000000        = T_f0                
 6.000000        = T_V0                
 6.000000        = T_V0                
 1.700000        = T_p                 
 1.700000        = T_p                 
 11.000000       = T_VL                
 11.000000       = T_VL                
 0.140000        = b1                  
 0.140000        = b1                  
 0.530000        = b2                  
 0.530000        = b2                  
 5.000000        = b5                  
 5.000000        = b5                  
 0.300000        = A1                  
 0.300000        = A1                  
 0.700000        = A2                  
 0.700000        = A2                  
 1.000000        = A5                  
 1.000000        = A5                  
 0.000000        = S1                  
 0.000000        = S2                  
 0.000000        = S3                  
 0.000000        = S4                  
 1.414400        = Cn1                 
 -0.532400       = Cn2                 
 0.190000        = St_sh               
 0.190000        = St_sh               
 0.006000        = Cd0                 
 -0.121000       = Cm0                 
 0.000000        = k0                  
 0.000000        = k1                  
 0.000000        = k2                  
 0.000000        = k3                  
 0.000000        = k1_hat              
 0.200000        = x_cp_bar            
 0.200000        = x_cp_bar            
 DEFAULT         = UACutout            
 DEFAULT         = filtCutOff          
 142             = NumAlf              
-1.80000000000000e+02  0.00000000000000e+00  1.85000000000000e-02  0.00000000000000e+00
-1.75000000000000e+02  3.94000000000000e-01  3.32000000000000e-02  1.97800000000000e-01
-1.70000000000000e+02  7.88000000000000e-01  9.45000000000000e-02  3.96300000000000e-01
-1.60000000000000e+02  6.70000000000000e-01  2.80900000000000e-01  2.73800000000000e-01
-1.55000000000000e+02  7.49000000000000e-01  3.93200000000000e-01  3.11800000000000e-01
-1.50000000000000e+02  7.97000000000000e-01  5.11200000000000e-01  3.41300000000000e-01
-1.45000000000000e+02  8.18000000000000e-01  6.30900000000000e-01  3.63600000000000e-01
-1.40000000000000e+02  8.13000000000000e-01  7.48500000000000e-01  3.79900000000000e-01
-1.35000000000000e+02  7.86000000000000e-01  8.61200000000000e-01  3.91100000000000e-01
-1.30000000000000e+02  7.39000000000000e-01  9.66500000000000e-01  3.98000000000000e-01
-1.25000000000000e+02  6.75000000000000e-01  1.06250000000000e+00  4.01200000000000e-01
-1.20000000000000e+02  5.96000000000000e-01  1.14760000000000e+00  4.01400000000000e-01
-1.15000000000000e+02  5.05000000000000e-01  1.22060000000000e+00  3.99000000000000e-01
-1.10000000000000e+02  4.03000000000000e-01  1.28050000000000e+00  3.94300000000000e-01
-1.05000000000000e+02  2.94000000000000e-01  1.32650000000000e+00  3.87800000000000e-01
-1.00000000000000e+02  1.79000000000000e-01  1.35820000000000e+00  3.79600000000000e-01
-9.50000000000000e+01  6.00000000000000e-02  1.37520000000000e+00  3.70000000000000e-01
-9.00000000000000e+01 -6.00000000000000e-02  1.37740000000000e+00  3.59100000000000e-01
-8.50000000000000e+01 -1.79000000000000e-01  1.36480000000000e+00  3.47100000000000e-01
-8.00000000000000e+01 -2.95000000000000e-01  1.33760000000000e+00  3.34000000000000e-01
-7.50000000000000e+01 -4.07000000000000e-01  1.29620000000000e+00  3.19900000000000e-01
-7.00000000000000e+01 -5.12000000000000e-01  1.24090000000000e+00  3.04900000000000e-01
-6.50000000000000e+01 -6.08000000000000e-01  1.17250000000000e+00  2.89000000000000e-01
-6.00000000000000e+01 -6.93000000000000e-01  1.09190000000000e+00  2.72200000000000e-01
-5.50000000000000e+01 -7.64000000000000e-01  1.00020000000000e+00  2.54500000000000e-01
-5.00000000000000e+01 -8.20000000000000e-01  8.99000000000000e-01  2.35900000000000e-01
-4.50000000000000e+01 -8.57000000000000e-01  7.90000000000000e-01  2.16300000000000e-01
-4.00000000000000e+01 -8.75000000000000e-01  6.75400000000000e-01  1.95800000000000e-01
-3.50000000000000e+01 -8.69000000000000e-01  5.57900000000000e-01  1.74400000000000e-01
-3.00000000000000e+01 -8.38000000000000e-01  4.40500000000000e-01  1.52000000000000e-01
-2.50000000000000e+01 -7.91000000000000e-01  3.25600000000000e-01  1.26200000000000e-01
-2.40000000000000e+01 -7.94000000000000e-01  3.01300000000000e-01  1.17000000000000e-01
-2.30000000000000e+01 -8.05000000000000e-01  2.76200000000000e-01  1.05900000000000e-01
-2.20000000000000e+01 -8.21000000000000e-01  2.50600000000000e-01  9.31000000000000e-02
-2.10000000000000e+01 -8.43000000000000e-01  2.24600000000000e-01  7.88000000000000e-02
-2.00000000000000e+01 -8.69000000000000e-01  1.98300000000000e-01  6.31000000000000e-02
-1.90000000000000e+01 -8.99000000000000e-01  1.72000000000000e-01  4.64000000000000e-02
-1.80000000000000e+01 -9.31000000000000e-01  1.45700000000000e-01  2.86000000000000e-02
-1.70000000000000e+01 -9.64000000000000e-01  1.19700000000000e-01  1.02000000000000e-02
-1.60000000000000e+01 -9.99000000000000e-01  9.40000000000000e-02 -8.80000000000000e-03
-1.50000000000000e+01 -1.03300000000000e+00  6.89000000000000e-02 -2.81000000000000e-02
-1.45000000000000e+01 -1.05000000000000e+00  5.67000000000000e-02 -3.78000000000000e-02
-1.20100000000000e+01 -9.53000000000000e-01  2.71000000000000e-02 -3.49000000000000e-02
-1.10000000000000e+01 -9.00000000000000e-01  3.03000000000000e-02 -3.61000000000000e-02
-9.98000000000000e+00 -8.27000000000000e-01  2.87000000000000e-02 -4.64000000000000e-02
-8.12000000000000e+00 -5.36000000000000e-01  1.24000000000000e-02 -8.21000000000000e-02
-7.62000000000000e+00 -4.67000000000000e-01  1.09000000000000e-02 -9.24000000000000e-02
-7.11000000000000e+00 -3.93000000000000e-01  9.20000000000000e-03 -1.01500000000000e-01
-6.60000000000000e+00 -3.23000000000000e-01  8.30000000000000e-03 -1.07300000000000e-01
-6.50000000000000e+00 -3.11000000000000e-01  8.90000000000000e-03 -1.08300000000000e-01
-6.00000000000000e+00 -2.45000000000000e-01  8.20000000000000e-03 -1.11200000000000e-01
-5.50000000000000e+00 -1.78000000000000e-01  7.40000000000000e-03 -1.14600000000000e-01
-5.00000000000000e+00 -1.13000000000000e-01  6.90000000000000e-03 -1.17200000000000e-01
-4.50000000000000e+00 -4.80000000000000e-02  6.50000000000000e-03 -1.19400000000000e-01
-4.00000000000000e+00  1.60000000000000e-02  6.30000000000000e-03 -1.21300000000000e-01
-3.50000000000000e+00  8.00000000000000e-02  6.10000000000000e-03 -1.23200000000000e-01
-3.00000000000000e+00  1.45000000000000e-01  5.80000000000000e-03 -1.25200000000000e-01
-2.50000000000000e+00  2.08000000000000e-01  5.70000000000000e-03 -1.26800000000000e-01
-2.00000000000000e+00  2.70000000000000e-01  5.70000000000000e-03 -1.28200000000000e-01
-1.50000000000000e+00  3.33000000000000e-01  5.70000000000000e-03 -1.29700000000000e-01
-1.00000000000000e+00  3.96000000000000e-01  5.70000000000000e-03 -1.31000000000000e-01
-5.00000000000000e-01  4.58000000000000e-01  5.70000000000000e-03 -1.32400000000000e-01
0.00000000000000e+00  5.21000000000000e-01  5.70000000000000e-03 -1.33700000000000e-01
5.00000000000000e-01  5.83000000000000e-01  5.70000000000000e-03 -1.35000000000000e-01
1.00000000000000e+00  6.45000000000000e-01  5.80000000000000e-03 -1.36300000000000e-01
1.50000000000000e+00  7.06000000000000e-01  5.80000000000000e-03 -1.37400000000000e-01
2.00000000000000e+00  7.68000000000000e-01  5.90000000000000e-03 -1.38500000000000e-01
2.50000000000000e+00  8.28000000000000e-01  6.10000000000000e-03 -1.39500000000000e-01
3.00000000000000e+00  8.88000000000000e-01  6.30000000000000e-03 -1.40300000000000e-01
3.50000000000000e+00  9.48000000000000e-01  6.60000000000000e-03 -1.40600000000000e-01
4.00000000000000e+00  9.96000000000000e-01  7.10000000000000e-03 -1.39800000000000e-01
4.50000000000000e+00  1.04600000000000e+00  7.90000000000000e-03 -1.39000000000000e-01
5.00000000000000e+00  1.09500000000000e+00  9.00000000000000e-03 -1.37800000000000e-01
5.50000000000000e+00  1.14500000000000e+00  1.03000000000000e-02 -1.36900000000000e-01
6.00000000000000e+00  1.19200000000000e+00  1.13000000000000e-02 -1.35300000000000e-01
6.50000000000000e+00  1.23900000000000e+00  1.22000000000000e-02 -1.33800000000000e-01
7.00000000000000e+00  1.28300000000000e+00  1.31000000000000e-02 -1.31700000000000e-01
7.50000000000000e+00  1.32400000000000e+00  1.39000000000000e-02 -1.29100000000000e-01
8.00000000000000e+00  1.35800000000000e+00  1.47000000000000e-02 -1.24900000000000e-01
8.50000000000000e+00  1.38500000000000e+00  1.58000000000000e-02 -1.21300000000000e-01
9.00000000000000e+00  1.40300000000000e+00  1.81000000000000e-02 -1.17700000000000e-01
9.50000000000000e+00  1.40100000000000e+00  2.11000000000000e-02 -1.14200000000000e-01
1.00000000000000e+01  1.35800000000000e+00  2.55000000000000e-02 -1.10300000000000e-01
1.05000000000000e+01  1.31300000000000e+00  3.01000000000000e-02 -1.06600000000000e-01
1.10000000000000e+01  1.28700000000000e+00  3.47000000000000e-02 -1.03200000000000e-01
1.15000000000000e+01  1.27400000000000e+00  4.01000000000000e-02 -1.00200000000000e-01
1.20000000000000e+01  1.27200000000000e+00  4.68000000000000e-02 -9.71000000000000e-02
1.25000000000000e+01  1.27300000000000e+00  5.45000000000000e-02 -9.40000000000000e-02
1.30000000000000e+01  1.27300000000000e+00  6.33000000000000e-02 -9.09000000000000e-02
1.35000000000000e+01  1.27300000000000e+00  7.22000000000000e-02 -8.83000000000000e-02
1.40000000000000e+01  1.27200000000000e+00  8.06000000000000e-02 -8.65000000000000e-02
1.45000000000000e+01  1.27300000000000e+00  9.00000000000000e-02 -8.54000000000000e-02
1.50000000000000e+01  1.27500000000000e+00  9.87000000000000e-02 -8.49000000000000e-02
1.55000000000000e+01  1.28100000000000e+00  1.07500000000000e-01 -8.47000000000000e-02
1.60000000000000e+01  1.28400000000000e+00  1.17000000000000e-01 -8.50000000000000e-02
1.65000000000000e+01  1.29600000000000e+00  1.27000000000000e-01 -8.58000000000000e-02
1.70000000000000e+01  1.30600000000000e+00  1.36800000000000e-01 -8.69000000000000e-02
1.75000000000000e+01  1.30800000000000e+00  1.46400000000000e-01 -8.83000000000000e-02
1.80000000000000e+01  1.30800000000000e+00  1.56200000000000e-01 -9.01000000000000e-02
1.85000000000000e+01  1.30800000000000e+00  1.66400000000000e-01 -9.22000000000000e-02
1.90000000000000e+01  1.30800000000000e+00  1.77000000000000e-01 -9.49000000000000e-02
1.95000000000000e+01  1.30700000000000e+00  1.87800000000000e-01 -9.80000000000000e-02
2.00000000000000e+01  1.31100000000000e+00  1.98700000000000e-01 -1.01700000000000e-01
2.05000000000000e+01  1.32500000000000e+00  2.10000000000000e-01 -1.05900000000000e-01
2.10000000000000e+01  1.32400000000000e+00  2.21400000000000e-01 -1.10500000000000e-01
2.20000000000000e+01  1.27700000000000e+00  2.49900000000000e-01 -1.17200000000000e-01
2.30000000000000e+01  1.22900000000000e+00  2.78600000000000e-01 -1.23900000000000e-01
2.40000000000000e+01  1.18200000000000e+00  3.07700000000000e-01 -1.30500000000000e-01
2.50000000000000e+01  1.13600000000000e+00  3.37100000000000e-01 -1.37000000000000e-01
2.60000000000000e+01  1.09300000000000e+00  3.66400000000000e-01 -1.43300000000000e-01
2.80000000000000e+01  1.01700000000000e+00  4.24600000000000e-01 -1.55600000000000e-01
3.00000000000000e+01  9.62000000000000e-01  4.81300000000000e-01 -1.67100000000000e-01
3.20000000000000e+01  9.37000000000000e-01  5.35600000000000e-01 -1.77800000000000e-01
3.50000000000000e+01  9.47000000000000e-01  6.12700000000000e-01 -1.92300000000000e-01
4.00000000000000e+01  9.50000000000000e-01  7.39600000000000e-01 -2.15400000000000e-01
4.50000000000000e+01  9.28000000000000e-01  8.62300000000000e-01 -2.37400000000000e-01
5.00000000000000e+01  8.84000000000000e-01  9.78100000000000e-01 -2.58300000000000e-01
5.50000000000000e+01  8.21000000000000e-01  1.08460000000000e+00 -2.78200000000000e-01
6.00000000000000e+01  7.40000000000000e-01  1.17960000000000e+00 -2.97100000000000e-01
6.50000000000000e+01  6.46000000000000e-01  1.26170000000000e+00 -3.14900000000000e-01
7.00000000000000e+01  5.40000000000000e-01  1.32970000000000e+00 -3.31800000000000e-01
7.50000000000000e+01  4.25000000000000e-01  1.38270000000000e+00 -3.47600000000000e-01
8.00000000000000e+01  3.04000000000000e-01  1.42020000000000e+00 -3.62500000000000e-01
8.50000000000000e+01  1.79000000000000e-01  1.44230000000000e+00 -3.76300000000000e-01
9.00000000000000e+01  5.30000000000000e-02  1.45120000000000e+00 -3.89000000000000e-01
9.50000000000000e+01 -7.30000000000000e-02  1.44800000000000e+00 -4.00400000000000e-01
1.00000000000000e+02 -1.98000000000000e-01  1.42940000000000e+00 -4.10500000000000e-01
1.05000000000000e+02 -3.19000000000000e-01  1.39540000000000e+00 -4.19100000000000e-01
1.10000000000000e+02 -4.34000000000000e-01  1.34640000000000e+00 -4.26000000000000e-01
1.15000000000000e+02 -5.41000000000000e-01  1.28290000000000e+00 -4.30800000000000e-01
1.20000000000000e+02 -6.37000000000000e-01  1.20570000000000e+00 -4.33300000000000e-01
1.25000000000000e+02 -7.20000000000000e-01  1.11570000000000e+00 -4.33000000000000e-01
1.30000000000000e+02 -7.87000000000000e-01  1.01440000000000e+00 -4.29400000000000e-01
1.35000000000000e+02 -8.36000000000000e-01  9.03300000000000e-01 -4.21900000000000e-01
1.40000000000000e+02 -8.64000000000000e-01  7.84500000000000e-01 -4.09800000000000e-01
1.45000000000000e+02 -8.69000000000000e-01  6.60500000000000e-01 -3.92200000000000e-01
1.50000000000000e+02 -8.47000000000000e-01  5.34600000000000e-01 -3.68200000000000e-01
1.55000000000000e+02 -7.95000000000000e-01  4.10300000000000e-01 -3.36400000000000e-01
1.60000000000000e+02 -7.11000000000000e-01  2.92200000000000e-01 -2.95400000000000e-01
1.70000000000000e+02 -7.88000000000000e-01  9.69000000000000e-02 -3.96600000000000e-01
1.75000000000000e+02 -3.94000000000000e-01  3.34000000000000e-02 -1.97800000000000e-01
1.80000000000000e+02  0.00000000000000e+00  1.85000000000000e-02  0.00000000000000e+00
--
Contents of "C:\Users\james\Desktop\WISDEM\OutputSimulationFiles\ws4.0\Airfoils\t1_AeroDyn15_Polar_07.dat":
 DEFAULT         = InterpOrd           
 1.0             = NonDimArea          
 401             = NumCoords           
0.250000       0
1.00000000000000e+00  0.00000000000000e+00
9.90000000000000e-01  3.38500000000000e-03
9.80000000000000e-01  6.12600000000000e-03
9.75000000000000e-01  7.44700000000000e-03
9.70000000000000e-01  8.76700000000000e-03
9.65000000000000e-01  1.00620000000000e-02
9.60000000000000e-01  1.13570000000000e-02
9.55000000000000e-01  1.26390000000000e-02
9.50000000000000e-01  1.39210000000000e-02
9.45000000000000e-01  1.52000000000000e-02
9.40000000000000e-01  1.64780000000000e-02
9.35000000000000e-01  1.77570000000000e-02
9.30000000000000e-01  1.90360000000000e-02
9.25000000000000e-01  2.03170000000000e-02
9.20000000000000e-01  2.15980000000000e-02
9.15000000000000e-01  2.28810000000000e-02
9.10000000000000e-01  2.41630000000000e-02
9.05000000000000e-01  2.54480000000000e-02
9.00000000000000e-01  2.67330000000000e-02
8.87500000000000e-01  2.99510000000000e-02
8.75000000000000e-01  3.31690000000000e-02
8.62500000000000e-01  3.63860000000000e-02
8.50000000000000e-01  3.96030000000000e-02
8.37500000000000e-01  4.28040000000000e-02
8.25000000000000e-01  4.60040000000000e-02
8.12500000000000e-01  4.91710000000000e-02
8.00000000000000e-01  5.23370000000000e-02
7.87500000000000e-01  5.54520000000000e-02
7.75000000000000e-01  5.85660000000000e-02
7.62500000000000e-01  6.16110000000000e-02
7.50000000000000e-01  6.46560000000000e-02
7.37500000000000e-01  6.76150000000000e-02
7.25000000000000e-01  7.05730000000000e-02
7.12500000000000e-01  7.34290000000000e-02
7.00000000000000e-01  7.62850000000000e-02
6.87500000000000e-01  7.90290000000000e-02
6.75000000000000e-01  8.17730000000000e-02
6.62500000000000e-01  8.43930000000000e-02
6.50000000000000e-01  8.70120000000000e-02
6.37500000000000e-01  8.94900000000000e-02
6.25000000000000e-01  9.19670000000000e-02
6.12500000000000e-01  9.42830000000000e-02
6.00000000000000e-01  9.65990000000000e-02
5.87500000000000e-01  9.87430000000000e-02
5.75000000000000e-01  1.00887000000000e-01
5.62500000000000e-01  1.02843000000000e-01
5.50000000000000e-01  1.04799000000000e-01
5.37500000000000e-01  1.06549000000000e-01
5.25000000000000e-01  1.08299000000000e-01
5.12500000000000e-01  1.09830000000000e-01
5.00000000000000e-01  1.11360000000000e-01
4.87500000000000e-01  1.12649000000000e-01
4.75000000000000e-01  1.13937000000000e-01
4.62500000000000e-01  1.14964000000000e-01
4.50000000000000e-01  1.15990000000000e-01
4.45000000000000e-01  1.16320000000000e-01
4.40000000000000e-01  1.16650000000000e-01
4.35000000000000e-01  1.16931000000000e-01
4.30000000000000e-01  1.17211000000000e-01
4.25000000000000e-01  1.17439000000000e-01
4.20000000000000e-01  1.17667000000000e-01
4.15000000000000e-01  1.17835000000000e-01
4.10000000000000e-01  1.18003000000000e-01
4.05000000000000e-01  1.18104000000000e-01
4.00000000000000e-01  1.18204000000000e-01
3.95000000000000e-01  1.18231000000000e-01
3.90000000000000e-01  1.18258000000000e-01
3.85000000000000e-01  1.18213000000000e-01
3.80000000000000e-01  1.18168000000000e-01
3.75000000000000e-01  1.18057000000000e-01
3.70000000000000e-01  1.17946000000000e-01
3.65000000000000e-01  1.17777000000000e-01
3.60000000000000e-01  1.17607000000000e-01
3.55000000000000e-01  1.17383000000000e-01
3.50000000000000e-01  1.17159000000000e-01
3.45000000000000e-01  1.16881000000000e-01
3.40000000000000e-01  1.16603000000000e-01
3.35000000000000e-01  1.16273000000000e-01
3.30000000000000e-01  1.15942000000000e-01
3.25000000000000e-01  1.15562000000000e-01
3.20000000000000e-01  1.15181000000000e-01
3.15000000000000e-01  1.14750000000000e-01
3.10000000000000e-01  1.14319000000000e-01
3.05000000000000e-01  1.13838000000000e-01
3.00000000000000e-01  1.13356000000000e-01
2.95000000000000e-01  1.12824000000000e-01
2.90000000000000e-01  1.12292000000000e-01
2.85000000000000e-01  1.11710000000000e-01
2.80000000000000e-01  1.11127000000000e-01
2.75000000000000e-01  1.10495000000000e-01
2.70000000000000e-01  1.09863000000000e-01
2.65000000000000e-01  1.09180000000000e-01
2.60000000000000e-01  1.08497000000000e-01
2.55000000000000e-01  1.07762000000000e-01
2.50000000000000e-01  1.07027000000000e-01
2.45000000000000e-01  1.06241000000000e-01
2.40000000000000e-01  1.05454000000000e-01
2.35000000000000e-01  1.04614000000000e-01
2.30000000000000e-01  1.03774000000000e-01
2.25000000000000e-01  1.02880000000000e-01
2.20000000000000e-01  1.01985000000000e-01
2.15000000000000e-01  1.01035000000000e-01
2.10000000000000e-01  1.00084000000000e-01
2.05000000000000e-01  9.90760000000000e-02
2.00000000000000e-01  9.80680000000000e-02
1.95000000000000e-01  9.70010000000000e-02
1.90000000000000e-01  9.59340000000000e-02
1.85000000000000e-01  9.48050000000000e-02
1.80000000000000e-01  9.36760000000000e-02
1.75000000000000e-01  9.24840000000000e-02
1.70000000000000e-01  9.12910000000000e-02
1.65000000000000e-01  9.00320000000000e-02
1.60000000000000e-01  8.87720000000000e-02
1.55000000000000e-01  8.74410000000000e-02
1.50000000000000e-01  8.61100000000000e-02
1.45000000000000e-01  8.47040000000000e-02
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1.60000000000000e+02 -7.14000000000000e-01  2.93100000000000e-01 -2.94200000000000e-01
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1.75000000000000e+02 -3.74000000000000e-01  3.34000000000000e-02 -1.87900000000000e-01
1.80000000000000e+02  0.00000000000000e+00  1.98000000000000e-02  0.00000000000000e+00
James-Ilosta commented 9 months ago

@James-Ilosta, which version of OpenFAST are your running?

I'm running V3.5.0

James-Ilosta commented 9 months ago

@jjonkman @andrew-platt I believe I may have found the source of the issue. I've been using FAST_writer.py located within ROSCO_toolbox>ofTools>fast_io to handle generating the input files for each of my simulations. As far as I can tell it generates an older file verison for ElastoDyn (ELASTODYN v1.03.* INPUT FILE).

This writer doesn't have a section in the output variables for generating node values. Therefore when I try to add in the nodal outputs into my initial ElastoDyn file, they are never copied into the new input file used to generate the simulation results.

Seems as though this is a ROSCO issue

jjonkman commented 9 months ago

@James-Ilosta,

The nodal outputs section of ElastoDyn is optional, so, just because ROSCO doesn't generate it doesn't mean that is in incorrect.

Regarding AeroDyn, is the Echo file that you are showing for AeroDyn generated by the AeroDyn input file you shared earlier? Because I don't see that the data is consistent, e.g. TwOutNd is different and the OutList variables you list in the input file are not included in the Echo file.

Best regards,