Closed eletroinf closed 3 years ago
jjonkman
commented
3 years ago Dear @eletroinf,
It looks like MATLAB is complaining about the following expression in your Simulink model despite that you have LSSTipPxa as an output from ElastoDyn.
u(strmatch('LSSTipPxa',OutList))
Does your model run without error if you run the open-loop version of the Simulink model, without feedback of output to input in Simulink?
Best regards,
bjonkman
commented
3 years ago Another thing you can check is if the 'LSSTipPxa' channel is specified in the list of channels being generated by OpenFAST. Take a look at the OutList variable in Matlab that is initialized from the FAST S-Function: this should match the list of variables that are printed in the OpenFAST summary file from your simulation. Note that the capitalization of the channel name that you specify in ElastoDyn must be the same as what you are searching for in the Simulink model, or the strmatch function won't find it.
eletroinf
commented
3 years ago Thank you for the answer and suggestions.
According with my Fast and now OpenFAST experience, this specific variable is being explicited (LSSTipPxa) is because it is the first variable in the ElastoDyn OutList. It means if I remove this variable from Simulink usage, it will result in a error pointing to the next variable of the OutList (BldPitch1) and so on.
I will make the suggested test anyway, but it happens that it is not the problem. This exact configuration works fine in OpenFAST 2.3.0 and in FAST 8.
eletroinf
commented
3 years ago Dear @jjonkman and @bjonkman
I ran the "Run_OpenLoop.m" in the examples folder and I got the output in the atached image.
jjonkman
commented
3 years ago Dear @eletroinf,
Is the actual error reported somewhere?
Best regards,
eletroinf
commented
3 years ago Dear @jjonkman
According my knowlege the error should be reported in this screen. But this image from the Matlab output is only what I have. There are another computer folder/file where I can search for OpenFAST error reports?
Thank you for the help!
bjonkman
commented
3 years ago There is a bug in the main branch (v2.5.0?) that overwrites the error message when the S-Function closes, so it doesn't print what the error was. That was fixed in the current dev branch with pull request https://github.com/OpenFAST/openfast/pull/641.
eletroinf
commented
3 years ago Dear @bjonkman and @jjonkman
I compiled the dev version and now I could see the error. Thanks for the quick response, now I think I can figure out what is happening.
Error using test13_fast_v10_automated_test (line 45) Error due to multiple causes. Caused by: Error using test13_fast_v10_automated_test (line 45) Error reported by S-function 'FAST_SFunc' in 'test13_fast_v10_rmrac_ipc_col/FAST Nonlinear Wind Turbine/S-Function': FAST_InitializeAll:AD_Init:ParsePrimaryFileInfo:ParseInVar:
A fatal error occurred when parsing data from "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/WP_Baseline_AeroDyn15_Dynin.dat". The variable "TwrShadow" was not assigned valid INTEGER value on line #9. The text being parsed was : "False TwrShadow - Calculate tower influence on wind based on downstream tower shadow? (flag)" Error using test13_fast_v10_automated_test (line 45) The expression: u(strmatch('LSSTipPxa',OutList)) in 'test13_fast_v10_rmrac_ipc_col/IPC dq/Azimuth' has a syntax error
eletroinf
commented
3 years ago I updated my Aerodyn and Elastodyn according OpenFAST-dev r-test and now I am getting the following error: "FAST_Start:size of NumOutputs is invalid"
Any suggestion to solve that?
Your guidance is so helpful. Thank you
`** OpenFAST
Copyright (C) 2021 National Renewable Energy Laboratory Copyright (C) 2021 Envision Energy USA LTD
This program is licensed under Apache License Version 2.0 and comes with ABSOLUTELY NO WARRANTY. See the "LICENSE" file distributed with this software for details.
OpenFAST-Unversioned from 75571452ae7fe3c0cd6308eaec5e4e57d54b36f4 Compile Info:
Time: 21:09:59-0300
OpenFAST input file heading: FAST Certification Test #13: WindPACT 1.5 MW Baseline with many DOFs with VS and VP and FF turbulence.
Running ElastoDyn. Nodal outputs section of ElastoDyn input file not found or improperly formatted. Running AeroDyn. AD15 Nodal Outputs: Nodal output section of AeroDyn input file not found or improperly formatted. Skipping nodal outputs. Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 1, blade 1) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 2, blade 1) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 1, blade 2) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 2, blade 2) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 1, blade 3) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 2, blade 3) Running InflowWind.
Reading a 13x13 grid (80 m wide, 44.288 m to 124.29 m above ground) with a characteristic wind speed of 14.5 m/s.
Processed 12111 time steps of 20-Hz full-field data (605.5 seconds). Running ServoDyn. Time: 0 of 50 seconds.
OpenFAST completed.
Error using test13_fast_v10_automated_test (line 45) Error reported by S-function 'FAST_SFunc' in 'test13_fast_v10_rmrac_ipc_col/FAST Nonlinear Wind Turbine/S-Function':
FAST_Start:size of NumOutputs is invalid.
`
eletroinf
commented
3 years ago Another question. In docs, https://openfast.readthedocs.io/en/dev/source/user/api_change.html
It is written to add a column at line 61 of the Aerodyn15 input file, but 4 values are provided to TwrTi flag. How use them?
EDIT: I got how to solve this by means of OpenFAST-dev r-tests, except that the values in that file cause the message saying Aerodyn15 file are improperly formated.
My Aerodyn is like this:
====== Tower Influence and Aerodynamics ============================================================= [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True] 2 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True] TwrElev TwrDiam TwrCd TwrTi (m) (m) (-) 0.0000000E+00 5.6200000E+00 0.0000000E+00 0.0000000E+00 1.0000000E+00 8.2390000E+01 2.8200000E+00 0.0000000E+00 6.0000000E+00 1.0000000E-01
Is that correct? How put the additional 4 values in 1 column as stated?
Thanks!
jjonkman
commented
3 years ago Dear @eletroinf,
The error "NumOutputs is invalid" when using the dev branch of OpenFAST has been discussed recently in the following issue: https://github.com/OpenFAST/openfast/issues/692.
The table of tower aerodynamic analysis nodes in the AeroDyn primary input file previously had three columns (TwrElev, TwrDiam, and TwrCd), but recently in dev a fourth column was added (TwrElev, TwrDiam, TwrCd, and TwrTI). It looks like you have one to many columns.
Best regards,
eletroinf
commented
3 years ago I compiled the new OpenFAST-dev version now and it is working! Thank you all for the good job!
Best regards, Ricardo Morim
eletroinf
commented
3 years ago Only one more point. In my tests I figured out that the simulation are not able to overwrite the *ech files, generating an error when runing a second simulunation, like this:
Error using test13_fast_v10_automated_test (line 45) Error due to multiple causes. Caused by: Error using test13_fast_v10_automated_test (line 45) Error reported by S-function 'FAST_SFunc' in 'test13_fast_v10_rmrac_ipc_col/FAST Nonlinear Wind Turbine/S-Function': FAST_InitializeAll:AD_Init:ParsePrimaryFileInfo:OpenEcho:OpenFOutFile:Cannot open file "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/WP_VSP_WTurb.SFunc.AD.ech". Another program like MS Excel may have locked it for writing. Error using test13_fast_v10_automated_test (line 45) The expression: u(strmatch('Azimuth',OutList)) in 'test13_fast_v10_rmrac_ipc_col/IPC dq/Azimuth' has a syntax error
To solve this it is necessary to close the Matlab and reopen. Disabling the generation o echo files also solve the problem.
LaurenceWETI
commented
2 years ago Hello everyone,
I just compiled the latest OpenFAST version OpenFAST-v3.0.0-1-gebff1b46 and tried to run some test using the S-Function. unfortunately, I received the previous error that @eletroinf had.
Error using Run_OpenLoop (line 12)
Error reported by S-function 'FAST_SFunc' in 'OpenLoop/FAST Nonlinear
Wind Turbine/S-Function':
FAST_InitializeAll:FAST_Init:FAST_ReadPrimaryFile:Invalid logical
input for file
"C:\....\openfast\repo\openfast\reg_tests\r-test\glue-codes\openfast\5MW_Land_DLL_WTurb\5MW_Land_DLL_WTurb.fst"
occurred while trying to read SumPrint.As discussed here, I compiled the dev version and run the tests with the OpenFAST-v3.0.0-458-gd0d94fd7-dirty. The simulation completed without any errors. Does that mean that the new version of OpenFAST OpenFAST-v3.0.0-1-gebff1b46 still not available for the S-Function?
Best regards,
jjonkman
commented
2 years ago Hi @LaurenceWETI,
The error "invalid logical input for..." simply means that your input file is not compatible with the version of OpenFAST you are running. The changes in input file format with each version of OpenFAST are documented here: https://openfast.readthedocs.io/en/main/source/user/api_change.html. And to debug issues with input file formatting, you can enable the Echo option.
Best regards,
LaurenceWETI
commented
2 years ago Hello @jjonkman ,
Many thanks for your help. I could see in the echo that the input file reads the ENVIRONMENTAL CONDITIONS as the input file name of ED, BD AD etc. see the .ech file below:
This file of echoed input was generated by OpenFAST on 23-Feb-2022 at 16:48:23.
Data from OpenFAST primary input file "C:\Users\Alhrshy\Desktop\Promotion\2022\OpenFAST\Compiling_OpenFAST\openfast\repo\openfast\reg_tests\r-test\glue-codes\openfast\5MW_Land_DLL_WTurb\5MW_Land_DLL_WTurb.fst":
FTitle - File Header: File Description (line 2)
"FAST Certification Test #18: NREL 5.0 MW Baseline Wind Turbine (Onshore)"
T Echo - Echo input data to <RootName>.ech (flag)
AbortLevel - Error level when simulation should abort (string)
"FATAL"
6.0000E+01 TMax - Total run time (s)
6.2500E-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}
0 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}
EDFile - Name of file containing ElastoDyn input parameters (-)
"----------------------"
BDBldFile(1) - Name of file containing BeamDyn blade 1input parameters (-)
"9.80665"
BDBldFile(2) - Name of file containing BeamDyn blade 2input parameters (-)
"1.225"
BDBldFile(3) - Name of file containing BeamDyn blade 3input parameters (-)
"0"
InflowFile - Name of file containing inflow wind input parameters (-)
"1.464E-05"
AeroFile - Name of file containing aerodynamic input parameters (-)
"335"
ServoFile - Name of file containing control and electrical-drive input parameters (-)
"103500"
HydroFile - Name of file containing hydrodynamic input parameters (-)
"1700"
SubFile - Name of file containing sub-structural input parameters (-)
"0"
MooringFile - Name of file containing mooring system input parameters (-)
"0"
IceFile - Name of file containing ice input parameters (-)
"----------------------"
do you know how could I fixe this error?
Best regards,
jjonkman
commented
2 years ago Dear @LaurenceWETI,
It looks like your OpenFAST primary (*.fst) input file has the environmental conditions section in it, but the version of OpenFAST you are using does not require that this section be included in that file. The environmental conditions section was added to the OpenFAST primary input file in the following PR, which was recently merged into the dev branch: https://github.com/OpenFAST/openfast/pull/707.
Best regards,
Hi I am facing problems in running my simulation (working fine in OpenFAST 2.3.0) in OpenFast 2.5.0. I am using Matlab/Simulink 2018b and I compiled OpenFast with Visual Studio and Intel Fortran Compilers.
Any suggestion about how to solve this?
That is what I am getting in Matlab 2018b output:
IPC active simulation
OpenFAST
Copyright (C) 2021 National Renewable Energy Laboratory Copyright (C) 2021 Envision Energy USA LTD
This program is licensed under Apache License Version 2.0 and comes with ABSOLUTELY NO WARRANTY. See the "LICENSE" file distributed with this software for details.
OpenFAST-Unversioned from 718d46f707d78e85edf1b49d3b1a63e8e23e1aae Compile Info:
Time: 11:16:52-0300
OpenFAST input file heading: FAST Certification Test #13: WindPACT 1.5 MW Baseline with many DOFs with VS and VP and FF turbulence.
Running ElastoDyn. Nodal outputs section of ElastoDyn input file not found or improperly formatted. Running AeroDyn. Nodal output section of AeroDyn input file not found or improperly formatted. Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 1, blade 1) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 2, blade 1) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 1, blade 2) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 2, blade 2) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 1, blade 3) Warning: Turning off Unsteady Aerodynamics because C_nalpha is 0. (node 2, blade 3) Running InflowWind.
OpenFAST completed.
Error using test13_fast_v10_automated_test (line 45) Error due to multiple causes. Caused by: Error using test13_fast_v10_automated_test (line 45) Error reported by S-function 'FAST_SFunc' in 'test13_fast_v10_rmrac_ipc_col/FAST Nonlinear Wind Turbine/S-Function': Error using test13_fast_v10_automated_test (line 45) The expression: u(strmatch('LSSTipPxa',OutList)) in 'test13_fast_v10_rmrac_ipc_col/IPC dq/Azimuth' has a syntax error
/** My Computer: Lenovo M920q, i5-8500T, 16 GB of RAM, Windows 10 x64. **/
/** Elastodyn Echo file **/
This file of echoed input was generated by ElastoDyn on 26-Mar-2021 at 11:16:52.
Data from ElastoDyn primary input file "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/WP_VSP_WTurb_ElastoDyn.dat":
"FAST certification Test #13: WindPACT 1.5 MW Baseline with many DOFs with VS and VP and FF turbulence. Model properties from "InputData1.5A08V07adm.xls" (from C. Hansen) with bugs removed."
"0.005"
9.8067E+00 Gravity - Gravitational acceleration (m/s^2)
0.0000E+00 OoPDefl - Initial out-of-plane blade-tip displacement (meters) 0.0000E+00 IPDefl - Initial in-plane blade-tip deflection (meters) 7.5000E+00 BlPitch(1) - Initial blade pitch angles (deg) 7.5000E+00 BlPitch(2) - Initial blade pitch angles (deg) 7.5000E+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) 1.0000E+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) 0.0000E+00 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)
3.5000E+01 TipRad - Preconed blade-tip radius (distance from the rotor apex to the blade tip) (meters) 1.7500E+00 HubRad - Preconed hub radius (distance from the rotor apex to the blade root) (meters) 0.0000E+00 PreCone(1) - Rotor precone angles (deg) 0.0000E+00 PreCone(2) - Rotor precone angles (deg) 0.0000E+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) -3.3000E+00 OverHang - Distance from yaw axis to rotor apex or teeter pin (meters) 9.9000E-01 ShftGagL - Distance from hub or teeter pin to shaft strain gages (meters) -5.0000E+00 ShftTilt - Rotor shaft tilt angle (deg) -1.4490E-01 NacCMxn - Downwind distance from tower-top to nacelle CM (meters) 0.0000E+00 NacCMyn - Lateral distance from tower-top to nacelle CM (meters) 1.3890E+00 NacCMzn - Vertical distance from tower-top to nacelle CM (meters) 0.0000E+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) 0.0000E+00 NcIMUzn - Vertical distance from the tower-top to the nacelle IMU (meters) 1.6100E+00 Twr2Shft - Vertical distance from the tower-top to the rotor shaft (meters) 8.2390E+01 TowerHt - Height of tower above ground level [onshore] or MSL [offshore] (meters) 0.0000E+00 TowerBsHt - Height of tower base above ground level [onshore] or MSL [offshore] (meters) 0.0000E+00 PtfmCMxt - Downwind distance from the ground [onshore] or MSL [offshore] to the platform CM (meters) 0.0000E+00 PtfmCMzt - Lateral distance from the ground [onshore] or MSL [offshore] to the platform CM (meters) 0.0000E+00 PtfmCMzt - Vertical distance from the ground [onshore] or MSL [offshore] to the platform CM (meters) 0.0000E+00 PtfmRefzt - Vertical distance from the ground [onshore] or MSL [offshore] 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) 1.5148E+04 HubMass - Hub mass (kg) 3.4600E+04 HubIner - Hub inertia about teeter axis (2-blader) or rotor axis (3-blader) (kg m^2) 5.3036E+01 GenIner - Generator inertia about HSS (kg m^2) 5.1170E+04 NacMass - Nacelle mass (kg) 4.9130E+04 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) 0.0000E+00 PtfmYIner - Platform inertia for yaw rotation about the platform CM (kg m^2)
1.5000E+01 BldNodes - Number of blade nodes (per blade) used for analysis (-) BldFile(1) - Name of the file containing properties for blade 1 "../WP_Baseline/Baseline_Blade.dat" BldFile(2) - Name of the file containing properties for blade 2 "../WP_Baseline/Baseline_Blade.dat" BldFile(3) - Name of the file containing properties for blade 3 "../WP_Baseline/Baseline_Blade.dat"
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 (%) 8.7965E+01 GBRatio - Gearbox ratio (-) 5.6000E+09 DTTorSpr - Drivetrain torsional spring (N-m/rad) 1.0000E+07 DTTorDmp - Drivetrain torsional damper (N-m/(rad/s))
"unused"
"../WP_Baseline/Baseline_Tower.dat"
"ES10.3E2" 0.0000E+00 Tstart - Time to start module's tabular output (seconds) 10 DecFact - Decimation factor for module's tabular output (1=output every step) (-) 2 NTwGages - Number of tower strain gages (-) TwrGagNd - Nodes closest to the tower strain gages (-) 4 7 0 NBlGages - Number of blade strain gages (-) BldGagNd - Nodes closest to the blade strain gages (-)
"LSSTipPxa" 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 "IPDefl1" OutList - List of user-requested output channels "IPDefl2" OutList - List of user-requested output channels "TwstDefl1" OutList - List of user-requested output channels "TwstDefl2" OutList - List of user-requested output channels "TwstDefl3" OutList - List of user-requested output channels "RootMxb1" OutList - List of user-requested output channels "RootMyb1" OutList - List of user-requested output channels "RootMzb1" OutList - List of user-requested output channels "RootMxb2" OutList - List of user-requested output channels "RootMyb2" OutList - List of user-requested output channels "RootMzb2" OutList - List of user-requested output channels "RootMxb3" OutList - List of user-requested output channels "RootMyb3" OutList - List of user-requested output channels "RootMzb3" OutList - List of user-requested output channels "LSShftFys" OutList - List of user-requested output channels "LSShftFzs" OutList - List of user-requested output channels "LSSTipMys" OutList - List of user-requested output channels "LSSTipMzs" OutList - List of user-requested output channels "LSSTipMya" OutList - List of user-requested output channels "LSSTipMza" OutList - List of user-requested output channels "YawBrTDxp" OutList - List of user-requested output channels "YawBrTDyp" OutList - List of user-requested output channels "YawBrMxn" OutList - List of user-requested output channels "YawBrMyn" OutList - List of user-requested output channels "YawBrMzn" OutList - List of user-requested output channels "LSSGagPxa" OutList - List of user-requested output channels "RotSpeed" OutList - List of user-requested output channels "PtfmPitch" OutList - List of user-requested output channels "PtfmYaw" OutList - List of user-requested output channels "LSSTipMzs" OutList - List of user-requested output channels "TwrBsMzt" OutList - List of user-requested output channels "TwrBsMyt" OutList - List of user-requested output channels "TwrBsMxt" OutList - List of user-requested output channels "RootFxb1" OutList - List of user-requested output channels "RootFxb2" OutList - List of user-requested output channels "RootFxb3" OutList - List of user-requested output channels "LSSGagFys" OutList - List of user-requested output channels "YawBrTAxp" OutList - List of user-requested output channels "YawBrTAyp" OutList - List of user-requested output channels "NcIMUTAxs" OutList - List of user-requested output channels "NcIMUTAys" OutList - List of user-requested output channels "LSShftMxa" OutList - List of user-requested output channels "TipDxb1" OutList - List of user-requested output channels "TipDyb1" OutList - List of user-requested output channels "TipDxb2" OutList - List of user-requested output channels "TipDyb2" OutList - List of user-requested output channels "TipDxb3" OutList - List of user-requested output channels "TipDyb3" OutList - List of user-requested output channels "GenSpeed" OutList - List of user-requested output channels "END"
Blade 1 input data from file "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/../WP_Baseline/Baseline_Blade.dat":
3.8820E+00 BldFlDmp(1) - Blade structural damping ratios in flapwise direction 3.8820E+00 BldFlDmp(2) - Blade structural damping ratios in flapwise direction 5.9000E+00 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 1.0000E+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
0.0000E+00 2.5000E-01 1.1100E+01 1.4476E+03 7.6815E+09 7.6815E+09 Line2 - Blade input station table 2.1050E-02 2.5000E-01 1.1100E+01 1.8033E+02 1.1699E+09 1.1699E+09 Line3 - Blade input station table 5.2630E-02 2.7100E-01 1.1100E+01 1.8167E+02 1.0206E+09 1.0923E+09 Line4 - Blade input station table 1.0526E-01 2.9900E-01 1.1100E+01 1.8390E+02 7.7188E+08 9.6297E+08 Line5 - Blade input station table 1.5789E-01 3.2100E-01 1.1100E+01 1.8614E+02 5.2314E+08 8.3366E+08 Line6 - Blade input station table 2.1053E-01 3.4000E-01 1.1100E+01 1.8837E+02 2.7440E+08 7.0435E+08 Line7 - Blade input station table 2.6316E-01 3.3500E-01 9.5000E+00 1.7832E+02 2.3457E+08 6.1465E+08 Line8 - Blade input station table 3.1579E-01 3.3000E-01 7.9000E+00 1.6827E+02 1.9474E+08 5.2496E+08 Line9 - Blade input station table 3.6842E-01 3.2400E-01 6.3000E+00 1.5822E+02 1.5490E+08 4.3526E+08 Line10 - Blade input station table 4.2105E-01 3.1700E-01 4.7000E+00 1.4817E+02 1.1507E+08 3.4557E+08 Line11 - Blade input station table 4.7368E-01 3.1000E-01 3.1000E+00 1.3812E+02 7.5230E+07 2.5587E+08 Line12 - Blade input station table 5.2632E-01 3.0600E-01 2.6000E+00 1.2290E+02 6.2490E+07 2.1787E+08 Line13 - Blade input station table 5.7895E-01 3.0000E-01 2.1000E+00 1.0767E+02 4.9750E+07 1.7986E+08 Line14 - Blade input station table 6.3158E-01 2.9500E-01 1.6000E+00 9.2442E+01 3.7010E+07 1.4186E+08 Line15 - Blade input station table 6.8421E-01 2.8800E-01 1.1000E+00 7.7215E+01 2.4270E+07 1.0385E+08 Line16 - Blade input station table 7.3684E-01 2.8000E-01 6.0000E-01 6.1988E+01 1.1530E+07 6.5850E+07 Line17 - Blade input station table 7.8947E-01 2.7600E-01 4.8000E-01 5.1861E+01 9.2700E+06 5.4250E+07 Line18 - Blade input station table 8.4211E-01 2.7100E-01 3.6000E-01 4.1734E+01 7.0100E+06 4.2660E+07 Line19 - Blade input station table 8.9474E-01 2.6600E-01 2.4000E-01 3.1607E+01 4.7500E+06 3.1060E+07 Line20 - Blade input station table 9.4737E-01 2.5900E-01 1.2000E-01 2.1480E+01 2.4900E+06 1.9470E+07 Line21 - Blade input station table 1.0000E+00 2.5000E-01 0.0000E+00 1.1353E+01 2.3000E+05 7.8700E+06
8.3800E-02 BldFl1Sh(1) - Blade-flap mode-1 shape coefficients 1.6525E+00 BldFl1Sh(2) - Blade-flap mode-1 shape coefficients -1.5682E+00 BldFl1Sh(3) - Blade-flap mode-1 shape coefficients 1.6947E+00 BldFl1Sh(4) - Blade-flap mode-1 shape coefficients -8.6280E-01 BldFl1Sh(5) - Blade-flap mode-1 shape coefficients -3.0080E-01 BldFl2Sh(1) - Blade-flap mode-2 shape coefficients -1.9968E+00 BldFl2Sh(2) - Blade-flap mode-2 shape coefficients -4.6564E+00 BldFl2Sh(3) - Blade-flap mode-2 shape coefficients 1.6966E+01 BldFl2Sh(4) - Blade-flap mode-2 shape coefficients -9.0121E+00 BldFl2Sh(5) - Blade-flap mode-2 shape coefficients 3.1650E-01 BldEdgSh(1) - Blade-edge mode shape coefficients 3.2618E+00 BldEdgSh(2) - Blade-edge mode shape coefficients -6.4005E+00 BldEdgSh(3) - Blade-edge mode shape coefficients 6.0367E+00 BldEdgSh(4) - Blade-edge mode shape coefficients -2.2146E+00 BldEdgSh(5) - Blade-edge mode shape coefficients
Tower input data from file "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/../WP_Baseline/Baseline_Tower.dat":
3.4350E+00 TwrFADmp(1) - Tower fore-aft structural damping ratios (%) 3.4350E+00 TwrFADmp(2) - Tower fore-aft structural damping ratios (%) 3.4350E+00 TwrSSDmp(1) - Tower side-to-side structural damping ratios (%) 3.4350E+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 (-)
0.0000E+00 2.5497E+03 2.4306E+11 2.4306E+11 Line2 - Tower input station table 1.1111E-01 2.2758E+03 1.9366E+11 1.9366E+11 Line3 - Tower input station table 2.2222E-01 2.0175E+03 1.5220E+11 1.5220E+11 Line4 - Tower input station table 3.3333E-01 1.7747E+03 1.1779E+11 1.1779E+11 Line5 - Tower input station table 4.4444E-01 1.5474E+03 8.9570E+10 8.9570E+10 Line6 - Tower input station table 5.5556E-01 1.3358E+03 6.6753E+10 6.6753E+10 Line7 - Tower input station table 6.6667E-01 1.1396E+03 4.8601E+10 4.8601E+10 Line8 - Tower input station table 7.7778E-01 9.5909E+02 3.4430E+10 3.4430E+10 Line9 - Tower input station table 8.8889E-01 7.9409E+02 2.3610E+10 2.3610E+10 Line10 - Tower input station table 1.0000E+00 6.4467E+02 1.5566E+10 1.5566E+10
7.6960E-01 TwFAM1Sh(1) - Tower fore-aft mode-1 shape coefficients (-) 4.2880E-01 TwFAM1Sh(2) - Tower fore-aft mode-1 shape coefficients (-) -5.3760E-01 TwFAM1Sh(3) - Tower fore-aft mode-1 shape coefficients (-) 7.6780E-01 TwFAM1Sh(4) - Tower fore-aft mode-1 shape coefficients (-) -4.2860E-01 TwFAM1Sh(5) - Tower fore-aft mode-1 shape coefficients (-) -2.6041E+01 TwFAM2Sh(1) - Tower fore-aft mode-2 shape coefficients (-) 1.3695E+01 TwFAM2Sh(2) - Tower fore-aft mode-2 shape coefficients (-) -5.6458E+00 TwFAM2Sh(3) - Tower fore-aft mode-2 shape coefficients (-) 5.2642E+01 TwFAM2Sh(4) - Tower fore-aft mode-2 shape coefficients (-) -3.3651E+01 TwFAM2Sh(5) - Tower fore-aft mode-2 shape coefficients (-)
7.6960E-01 TwSSM1Sh(1) - Tower side-to-side mode-1 shape coefficients (-) 4.2880E-01 TwSSM1Sh(2) - Tower side-to-side mode-1 shape coefficients (-) -5.3760E-01 TwSSM1Sh(3) - Tower side-to-side mode-1 shape coefficients (-) 7.6780E-01 TwSSM1Sh(4) - Tower side-to-side mode-1 shape coefficients (-) -4.2860E-01 TwSSM1Sh(5) - Tower side-to-side mode-1 shape coefficients (-) -2.6041E+01 TwSSM2Sh(1) - Tower side-to-side mode-2 shape coefficients (-) 1.3695E+01 TwSSM2Sh(2) - Tower side-to-side mode-2 shape coefficients (-) -5.6458E+00 TwSSM2Sh(3) - Tower side-to-side mode-2 shape coefficients (-) 5.2642E+01 TwSSM2Sh(4) - Tower side-to-side mode-2 shape coefficients (-) -3.3651E+01 TwSSM2Sh(5) - Tower side-to-side mode-2 shape coefficients (-)
/** AeroDyn Echo file **/
This file of echoed input was generated by AeroDyn on 26-Mar-2021 at 11:16:52.
Data from AeroDyn primary input file "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/WP_Baseline_AeroDyn15_Dynin.dat":
"1.5 MW baseline aerodynamic parameters for FAST certification tests #11-#13."
"default" 1 WakeMod - Type of wake/induction model {0=none, 1=BEMT, 2=DBEMT, 3=FVW} (-) 2 AFAeroMod - Type of airfoil aerodynamics model {1=steady model, 2=Beddoes-Leishman unsteady model} (-) 0 TwrPotent - Type tower influence on wind based on potential flow around the tower {0=none, 1=baseline potential flow, 2=potential flow with Bak correction} (-) F TwrShadow - Calculate tower influence on wind based on downstream tower shadow? (flag) F TwrAero - Calculate tower aerodynamic loads? (flag) F FrozenWake - Assume frozen wake during linearization? (flag) F CavitCheck - Perform cavitation check? (flag) F CompAA - Compute AeroAcoustics? (flag) AA_Inputfile - AeroAcoustics Input filename "unused"
1.2250E+00 AirDens - Air density (kg/m^3) 1.4639E-05 KinVisc - Kinematic air viscosity (m^2/s) 3.3500E+02 SpdSound - Speed of sound (m/s) 1.0350E+05 Patm - Atmospheric pressure (Pa) 1.7000E+03 Pvap - Vapour pressure of fluid (Pa) 5.0000E-01 FluidDepth - Water depth above mid-hub height (MHK only, for cavitation check) (m)
"default" T TipLoss - Use the Prandtl tip-loss model? (flag) [unused when WakeMod={0|3}] T HubLoss - Use the Prandtl hub-loss model? (flag) [unused when WakeMod={0|3}] T TanInd - Include tangential induction in BEMT calculations? (flag) [unused when WakeMod={0|3}] F AIDrag - Include the drag term in the axial-induction calculation? (flag) [unused when WakeMod={0|3}] F TIDrag - Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod={0|3} or TanInd=FALSE] IndToler - Convergence tolerance for BEM induction factors (-) [unused when WakeMod={0|3}] "Default" 1.0000E+02 MaxIter - Maximum number of iteration steps (-) [unused when WakeMod={0|3}]
4.0000E+00 tau1_const - time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1]
"unused"
1.0000E+00 InCol_Alfa - The column in the airfoil tables that contains the angle of attack (-) 2.0000E+00 InCol_Cl - The column in the airfoil tables that contains the lift coefficient (-) 3.0000E+00 InCol_Cd - The column in the airfoil tables that contains the drag coefficient (-) 0.0000E+00 InCol_Cm - The column in the airfoil tables that contains the pitching-moment coefficient; use zero if there is no Cm column (-) 0.0000E+00 InCol_Cpmin - The column in the airfoil tables that contains the drag coefficient; use zero if there is no Cpmin column (-) 4 NumAFfiles - Number of airfoil files used (-) AFNames(1) - Airfoil 1 file name "../WP_Baseline/Airfoils/cylinder.dat" AFNames(2) - Airfoil 2 file name "../WP_Baseline/Airfoils/s818_2703.dat" AFNames(3) - Airfoil 3 file name "../WP_Baseline/Airfoils/s825_2103.dat" AFNames(4) - Airfoil 4 file name "../WP_Baseline/Airfoils/s826_1603.dat"
"../WP_Baseline/WP_Baseline_AeroDyn_blade.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for blade 2 "../WP_Baseline/WP_Baseline_AeroDyn_blade.dat" ADBlFile(3) - Name of file containing distributed aerodynamic properties for blade 3 "../WP_Baseline/WP_Baseline_AeroDyn_blade.dat"
0.0000E+00 5.6200E+00 0.0000E+00 TwrNds - Properties for tower node 2. 8.2390E+01 2.8200E+00 0.0000E+00
"RtSkew" OutList - List of user-requested output channels "RtAeroCt" OutList - List of user-requested output channels "RtAeroCq" OutList - List of user-requested output channels "END"
0.0000 0.0000 0.0000 0.0000 11.1000 1.9490 1 1.1083 -0.0030 -0.0153 0.0000 11.1000 1.9490 1 3.3250 -0.0201 -0.1024 0.0000 11.1000 2.2690 2 5.5417 -0.0369 -0.1880 0.0000 11.1000 2.5890 2 7.7583 -0.0436 -0.2374 0.0000 10.4100 2.7430 2 9.9750 -0.0308 -0.2091 0.0000 8.3800 2.5780 2 12.1917 -0.0197 -0.1774 0.0000 6.3500 2.4120 2 14.4083 -0.0110 -0.1456 0.0000 4.3300 2.2470 2 16.6250 -0.0060 -0.1206 0.0000 2.8500 2.0820 3 18.8417 -0.0038 -0.0976 0.0000 2.2200 1.9160 3 21.0583 -0.0022 -0.0788 0.0000 1.5800 1.7510 3 23.2750 -0.0009 -0.0571 0.0000 0.9500 1.5850 3 25.4917 -0.0004 -0.0400 0.0000 0.5300 1.4270 3 27.7083 -0.0002 -0.0281 0.0000 0.3800 1.2780 3 29.9250 -0.0001 -0.0169 0.0000 0.2300 1.1290 4 32.1417 -0.0000 -0.0059 0.0000 0.0800 0.9800 4 33.2500 0.0000 0.0000 0.0000 0.0800 0.9800 4
0.0000 0.0000 0.0000 0.0000 11.1000 1.9490 1 1.1083 -0.0030 -0.0153 0.0000 11.1000 1.9490 1 3.3250 -0.0201 -0.1024 0.0000 11.1000 2.2690 2 5.5417 -0.0369 -0.1880 0.0000 11.1000 2.5890 2 7.7583 -0.0436 -0.2374 0.0000 10.4100 2.7430 2 9.9750 -0.0308 -0.2091 0.0000 8.3800 2.5780 2 12.1917 -0.0197 -0.1774 0.0000 6.3500 2.4120 2 14.4083 -0.0110 -0.1456 0.0000 4.3300 2.2470 2 16.6250 -0.0060 -0.1206 0.0000 2.8500 2.0820 3 18.8417 -0.0038 -0.0976 0.0000 2.2200 1.9160 3 21.0583 -0.0022 -0.0788 0.0000 1.5800 1.7510 3 23.2750 -0.0009 -0.0571 0.0000 0.9500 1.5850 3 25.4917 -0.0004 -0.0400 0.0000 0.5300 1.4270 3 27.7083 -0.0002 -0.0281 0.0000 0.3800 1.2780 3 29.9250 -0.0001 -0.0169 0.0000 0.2300 1.1290 4 32.1417 -0.0000 -0.0059 0.0000 0.0800 0.9800 4 33.2500 0.0000 0.0000 0.0000 0.0800 0.9800 4
0.0000 0.0000 0.0000 0.0000 11.1000 1.9490 1 1.1083 -0.0030 -0.0153 0.0000 11.1000 1.9490 1 3.3250 -0.0201 -0.1024 0.0000 11.1000 2.2690 2 5.5417 -0.0369 -0.1880 0.0000 11.1000 2.5890 2 7.7583 -0.0436 -0.2374 0.0000 10.4100 2.7430 2 9.9750 -0.0308 -0.2091 0.0000 8.3800 2.5780 2 12.1917 -0.0197 -0.1774 0.0000 6.3500 2.4120 2 14.4083 -0.0110 -0.1456 0.0000 4.3300 2.2470 2 16.6250 -0.0060 -0.1206 0.0000 2.8500 2.0820 3 18.8417 -0.0038 -0.0976 0.0000 2.2200 1.9160 3 21.0583 -0.0022 -0.0788 0.0000 1.5800 1.7510 3 23.2750 -0.0009 -0.0571 0.0000 0.9500 1.5850 3 25.4917 -0.0004 -0.0400 0.0000 0.5300 1.4270 3 27.7083 -0.0002 -0.0281 0.0000 0.3800 1.2780 3 29.9250 -0.0001 -0.0169 0.0000 0.2300 1.1290 4 32.1417 -0.0000 -0.0059 0.0000 0.0800 0.9800 4 33.2500 0.0000 0.0000 0.0000 0.0800 0.9800 4
Contents of "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/../WP_Baseline/Airfoils/cylinder.dat": DEFAULT = InterpOrd
1 = NonDimArea
0 = NumCoords
unused = BL_file
1 = NumTabs
0.75 = Re
0 = UserProp
True = InclUAdata
0 = alpha0
14 = alpha1
-14 = alpha2
1 = eta_e
0 = C_nalpha
Default = T_f0
Default = T_V0
Default = T_p
Default = T_VL
Default = b1
Default = b2
Default = b5
Default = A1
Default = A2
Default = A5
0 = S1
0 = S2
0 = S3
0 = S4
0 = Cn1
0 = Cn2
Default = St_sh
1 = Cd0
0 = Cm0
0 = k0
0 = k1
0 = k2
0 = k3
0 = k1_hat
Default = x_cp_bar
Default = UACutout
DEFAULT = filtCutOff
3 = NumAlf
-180.0 0.0 0.5 0.0 0.0 0.0 0.5 0.0 180.0 0.0 0.5 0.0
Contents of "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/../WP_Baseline/Airfoils/s818_2703.dat": DEFAULT = InterpOrd
1 = NonDimArea
0 = NumCoords
unused = BL_file
1 = NumTabs
4 = Re
0 = UserProp
True = InclUAdata
-5.31 = alpha0
12.5 = alpha1
-12.5 = alpha2
1 = eta_e
6.1084 = C_nalpha
Default = T_f0
Default = T_V0
Default = T_p
Default = T_VL
Default = b1
Default = b2
Default = b5
Default = A1
Default = A2
Default = A5
0 = S1
0 = S2
0 = S3
0 = S4
1.956 = Cn1
-0.8 = Cn2
Default = St_sh
0.0082 = Cd0
0 = Cm0
0 = k0
0 = k1
0 = k2
0 = k3
0 = k1_hat
Default = x_cp_bar
Default = UACutout
DEFAULT = filtCutOff
57 = NumAlf
-180.00 -0.170 0.0200 -170.00 0.640 0.0500 -160.00 0.840 0.3100 -150.00 1.080 0.6200 -140.00 1.150 0.9600 -130.00 1.090 1.3000 -120.00 0.880 1.5200 -110.00 0.600 1.6600 -100.00 0.310 1.7600 -90.00 0.000 1.8000 -80.00 -0.310 1.7600 -70.00 -0.600 1.6600 -60.00 -0.880 1.5200 -50.00 -1.090 1.3000 -40.00 -1.150 0.9600 -30.00 -1.080 0.6200 -20.00 -0.840 0.3100 -10.00 -0.640 0.0144 -8.00 -0.480 0.0124 -6.00 -0.090 0.0082 -5.00 0.020 0.0082 -4.00 0.130 0.0082 -3.00 0.240 0.0082 -2.00 0.350 0.0086 -1.00 0.460 0.0086 0.00 0.570 0.0087 1.00 0.670 0.0088 2.00 0.780 0.0090 3.00 0.890 0.0093 4.00 0.990 0.0096 5.00 1.100 0.0099 6.00 1.200 0.0103 7.00 1.310 0.0108 8.00 1.410 0.0113 9.00 1.510 0.0118 10.00 1.560 0.0194 11.00 1.610 0.0221 12.00 1.650 0.0245 13.00 1.650 0.0269 14.00 1.630 0.0296 15.00 1.620 0.0520 30.00 1.080 0.6200 40.00 1.150 0.9600 50.00 1.090 1.3000 60.00 0.880 1.5200 70.00 0.600 1.6600 80.00 0.310 1.7600 90.00 0.000 1.8000 100.00 -0.310 1.7600 110.00 -0.600 1.6600 120.00 -0.880 1.5200 130.00 -1.090 1.3000 140.00 -1.150 0.9600 150.00 -1.080 0.6200 160.00 -0.840 0.3100 170.00 -0.640 0.0500 180.00 -0.170 0.0200
Contents of "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/../WP_Baseline/Airfoils/s825_2103.dat": DEFAULT = InterpOrd
1 = NonDimArea
0 = NumCoords
unused = BL_file
1 = NumTabs
3 = Re
0 = UserProp
True = InclUAdata
-6.1 = alpha0
12.5 = alpha1
-12.5 = alpha2
1 = eta_e
6.18827 = C_nalpha
Default = T_f0
Default = T_V0
Default = T_p
Default = T_VL
Default = b1
Default = b2
Default = b5
Default = A1
Default = A2
Default = A5
0 = S1
0 = S2
0 = S3
0 = S4
2.0641 = Cn1
-0.8 = Cn2
Default = St_sh
0.0074 = Cd0
0 = Cm0
0 = k0
0 = k1
0 = k2
0 = k3
0 = k1_hat
Default = x_cp_bar
Default = UACutout
DEFAULT = filtCutOff
57 = NumAlf
-180.00 -0.170 0.0200 -170.00 0.640 0.0500 -160.00 0.840 0.3100 -150.00 1.080 0.6200 -140.00 1.150 0.9600 -130.00 1.090 1.3000 -120.00 0.880 1.5200 -110.00 0.600 1.6600 -100.00 0.310 1.7600 -90.00 0.000 1.8000 -80.00 -0.310 1.7600 -70.00 -0.600 1.6600 -60.00 -0.880 1.5200 -50.00 -1.090 1.3000 -40.00 -1.150 0.9600 -30.00 -1.080 0.6200 -20.00 -0.840 0.3100 -10.00 -0.640 0.0144 -8.00 -0.480 0.0124 -6.00 0.010 0.0074 -5.00 0.120 0.0075 -4.00 0.230 0.0077 -3.00 0.340 0.0078 -2.00 0.440 0.0080 -1.00 0.550 0.0082 0.00 0.660 0.0084 1.00 0.770 0.0086 2.00 0.880 0.0089 3.00 0.980 0.0091 4.00 1.090 0.0095 5.00 1.200 0.0098 6.00 1.300 0.0102 7.00 1.410 0.0107 8.00 1.490 0.0155 9.00 1.580 0.0179 10.00 1.660 0.0203 11.00 1.680 0.0250 12.00 1.700 0.0273 13.00 1.700 0.0297 14.00 1.680 0.0324 15.00 1.660 0.0520 30.00 1.080 0.6200 40.00 1.150 0.9600 50.00 1.090 1.3000 60.00 0.880 1.5200 70.00 0.600 1.6600 80.00 0.310 1.7600 90.00 0.000 1.8000 100.00 -0.310 1.7600 110.00 -0.600 1.6600 120.00 -0.880 1.5200 130.00 -1.090 1.3000 140.00 -1.150 0.9600 150.00 -1.080 0.6200 160.00 -0.840 0.3100 170.00 -0.640 0.0500 180.00 -0.170 0.0200
Contents of "D:/ricardo/documents/PROGRAMAS/nrel_open_fast/glue-codes/openfast/WP_VSP_WTurb/../WP_Baseline/Airfoils/s826_1603.dat": DEFAULT = InterpOrd
1 = NonDimArea
0 = NumCoords
unused = BL_file
1 = NumTabs
3 = Re
0 = UserProp
True = InclUAdata
-6.61 = alpha0
12 = alpha1
-12 = alpha2
1 = eta_e
6.16567 = C_nalpha
Default = T_f0
Default = T_V0
Default = T_p
Default = T_VL
Default = b1
Default = b2
Default = b5
Default = A1
Default = A2
Default = A5
0 = S1
0 = S2
0 = S3
0 = S4
2.0013 = Cn1
-0.8 = Cn2
Default = St_sh
0.0067 = Cd0
0 = Cm0
0 = k0
0 = k1
0 = k2
0 = k3
0 = k1_hat
Default = x_cp_bar
Default = UACutout
DEFAULT = filtCutOff
57 = NumAlf
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