modified Jan, 16, 2006 by Luke Grahame
Stringers are in 4 corners of fuselage, used smallest diameter for smallest moment of inertia
Spacing of stringers
Max Loading on Fuselage
Force Equation
Moment Equation (From front of fuselage)
Dimensions based off of wing spar
Margin of Safety
Stringers in bending are not critical compared to wing spar