Jason Kirk
Jason Kirk
I strongly support using the "correct" methodology here. A very well-documented (methodology docs and in code) correction factor to nacelle drag is probably the cleanest way to make sure we...
If we decide we'd rather not introduce a 4-depth hierarchy, just `Aircraft.Propeller.` is an alternative we can consider _edit: we now have support for hierarchies of arbitrary depth so Aircraft.Engine.Propeller...
resolved with #519
> Is this issue solved? No, `rho` is still being used in several places in the code
Our documented code standards state a preference for physical descriptions, so we should use `ANGLE_OF_ATTACK`
Marked as `wontfix` until future decisions on additional SGM feature enhancement
`2dof` was formally changed to `2DOF` in a recent push, which removes the immediate need for this fix. I'd still like to investigate this further, at a lower priority
I'd like to have plots vs. range - they seem more intuitive, if only for the reason it's what most aircraft designers are used to. Having access to both types...
The standard atmosphere component can be upgraded with correction factors for an arbitrary temperature delta. We can host our own version of that component, but that upgrade might want to...
Yeah, looks like there's a hole in our docs on available options for aero. Let me try and fill that gap here. Aerodynamics has many methodologies you can use during...