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Hi Tushar,
I've created a pull request with a new setup. Changes are:
- improved blockMeshDict; have a look at the new mesh
- standard NACA 0012 airfoil
- files and options for Spalart-Allmara…
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Internet publications are not having an item type crosswalked, this is breaking downstream processing.
This should be set in mods:genre:
```
field:type_of_work
…
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Pretty much the title. NACA ducts are the common slits/wells seen on various aircraft and race cars which are optimized for spilling air into the interior for cooling. I've tried to keep the body "wat…
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When I ran the case codes, I got that:
`
julia> begin
airfoil = naca4((2,4,1,2));
foil = Foil(airfoil);
V, α = 1.0, 3.0;
uniform = Uniform2D(V, α…
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* [x] vytvořit víčko airspeed senzoru držící PCB TFASPDIMU
* [x] Upravit stávající řešení pro nový snímač [TFASPDIMU02](https://github.com/ThunderFly-aerospace/TFASPDIMU02)
* [x] Vyřešit umístění TF…
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## Bug Description
Running an inviscid analysis on a NACA 0012 airfoil at 0 degrees angle of attack produces non-zero lift coefficient.
## Steps to Reproduce
```python
from aerosandbox import Ai…
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- [x] Spodní rámeček 888_1007
- [x] Spodní část držáku silentbloků 888_1008
- [x] Vybrat + otestovat správné silentbloky
- [x] Horní část držáku silentbloků
- [x] Implementace Airspeed #16
…
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The v1.0.x release has poor directional stability, and the tacked-on stop-gap solution with the strakes and cardboard additions should be folded into a larger set of fins which blend into what is curr…
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**Is your feature request related to a problem? Please describe.**
I am not sure if this is a bug or a feature.
I am trying to get rudders working in our stonefish simulation.
I remember you sugg…
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Hi,
Please provide the mesh file 'grid.bin' to run the naca0012 testcases in Euler and Navier-Stokes applications.