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Hi,
First of all, thank you for this amazing software. The performance is out of this world.
I'm trying to simulate a wingsuit at different angles of attack. I was using Ansys Fluent for this but …
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Hi,
**Describe the bug**
The aerodynamic twist is applied in the wrong direction according to right-hand rule (positive `twist` results in downwards rotation of airfoil). This is also inconsistent…
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same as NAca fil importer but for other foils.
import_coords -> coefficients from xfoil -> store in separate file
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**Describe the bug**
For optimising a symmetric NACA 0012 airfoil, SU2 does not detect the `AIRFOIL_THICKNESS` automatically as it does for the complete geometry.
When `SU2_GEO` is utilized, it…
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https://www.uniprot.org/uniprot/Q13765#family_and_domains
THis is an odd case I wondered if somehow the incorrect entry was annotated?
Uniprot describes as NACA.
The evidence I'm currently lo…
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Aerodynamický profil NACA má zřejmě nastaveno malé rozlišení, neboť jsou na vytištěném modelu viditelné zuby.
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Hello, I recently updated my R studio to the latest version, and I tried to re-run to the infercnv codes I previously ran successfully, and got the following error warning after "Centering and scaling…
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I'm trying to use the examples given to see how bladegen works, perhaps there are other renaming issues with BOSL2 that are making their way here.
I'm running the following code from the examples:
…
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**Describe the bug**
When I test my customed dataset with the following steps:
```python
python3 tools/test.py ./projects/configs/cam_radar/res50_cam_radar.py ./work_dirs/retinanet_r50_fpn_2x_coc…
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A vertical tail wing (of an aircraft, NACA 0012) is simulated in OpenVSP, 3.27.1-win64.
The angle in z (deflection) is changed from -10° to +10°
One would expect the results to be symmetric, however…