Iteration 1: Aspect Ratio

from unyt import m, mm

TODO: references

https://www.grc.nasa.gov/www/k-12/airplane/geom.html

Initial design

b = 3050*mm # wingspan
c = 200*mm # chord

S = b*c # wing area
AR = b**2/S # = b/c because it's a rectangle

AR

unyt_quantity(15.25, '(dimensionless)')

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.