Open samiamandyesican opened 1 month ago
"we need to use sine spacing on the right half of the wing (since once reflected across the y-z plane, sine spacing become cosine spacing)."
"This, however, would give incorrect results for the lateral stability derivatives so we have instead mirrored our geometry across the X-Z plane."
Should I use Paraview online or in situ, also wut is going on
What is this?
fc = fill((xc) -> 0, 2) # camberline function for each section
plz help me figure out julia shell
I wrote some functions for reference area and stuff, but I don't know how to do it if there's also a tail.
Weird velocities on tail