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```
DATCOM needs a designation as to which NACA Airfoil designation belongs to
which wing. This designation is done in the following format as an example:
NACA-W-6-66-012
NACA-H-6-66-009
NACA-V-6-66…
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I am using SU2 version 3.2.8. I have tried all the steady-state Euler and Navier-Stokes test cases and they worked fine. However, none of the demos for Rotating (NACA and CAradonna) are working. Both …
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Hi
I have made a neu for HiFiLES by Gambit.
but I failed to set the boundary conditions after many times trial
Could you send me an neu.file and the input file for the case (2D) NACA 0012 0° AoA?
m…
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```
The following request (generated by libiscsi's 0105_read10_invalid test) does
not bring a response from istgt:
iSCSI (SCSI Command)
Opcode: SCSI Command (0x01)
.0.. .... = I: Queued deli…
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Add/update these fields to the PostGIS Parks table for maintenance/output back into CartoDB Parks table.
Add:
- [x] `unit_region`
- [x] `unit_state`
- [x] `unit_url`
- [x] `created_by`
- [x] `updated…
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Basically L/D ratio for a blade. Make an updated version of the old diagram I used during my MS for turbine loading with high and low L/D.
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SU2_DOT seems to give wrong results. For example using the test case cont_adj_euler/naca0012.
Just use the continuous_adjoint.py script to test this.
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Hi,all
I have question about mesh.
1,why the amount of grid is so little that cannot keep Geometric shape.
2,when i use SA model,40000 mesh, The calculation time is very long.why?
3,In tecplot,why the…
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This would be at the optimal TSR.
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Just double-check that the NACA profile formulas are correct in the 3D models.