Iteration 1: Aspect Ratio
Iteration 1: Aspect Ratio#
from unyt import m, mm
b = 3050*mm # wingspan c = 200*mm # chord
S = b*c # wing area AR = b**2/S # = b/c because it's a rectangle
Hmmm ok this is a little much…
The higher the better obviously but I want to be realistic with the materials I plan to use (styrofoam & wood spar) which means <13 is probably a better starting point.