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Quite a few users are using phantom body tubes for the attachment of shapes that are created using the freeform fin function. The most common use of this technique seems to be for the imitation of Est…
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Which vortex filament paper or set of textbooks or materials is your code based on?
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I would normally expect the unsteady airfoil aerodynamics (UA) model of OpenFAST / AeroDyn to influence the variations of lift about the mean, but not to directly influence the mean lift itself. Howe…
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From #65:
> Well, the aircraft type is still messy. It is used to dispatch on different methods depending on the aircraft type itself and also, it is composed of other types that store current valu…
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Brainstorming about how to use the turbinesFoam library in conjunction with [SOWFA](https://github.com/NREL/SOWFA).
Ideas:
- turbinesFoam takes care of the actuator line modeling.
- SOWFA deals with …
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It would be nice to have "damping derivatives" results for the three main axis rotation rates (p,q,r). They can be stored in the CPACS file @ .../AeroMap[i]/aeroPerformanceMap/dampingDerivatives
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### Desired capability or behavior.
Add a new form factor relationship specifically for Nacelles to generate more accurate drag buildup.
FLOPS (and Aviary) uses the same form factor relationship f…
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I was trying to calculate the lift coefficient of a NACA4412 airfoil and I encountered the following error:
```julia
foil = naca4((4,4,1,2), 70)
uniform = Uniform2D(1.0, 4.0)
system = solve_case(
…
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i see that every showcase you have are for airplanes and helicopters, flying vehicles, i just want to know if i it would work in an arcade car game or an f-zero like game, to have aerodynamics for te…
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Hello, thank you for publishing the model, but I encountered two issues while using it:
1： May I ask how you handle the aerodynamic data of F16? I would like to change this model to a low fidelity mo…