how to calculate torque and moment in a swept back wing?
how to calculate torque and moment in a swept back wing?
(OP)
If I have a swept back wing:
1) how would I find a formula to represent the relationship between shear force and bending moment? (function of span location)
1) how would I find a formula to represent the relationship between shear force and bending moment? (function of span location)





RE: how to calculate torque and moment in a swept back wing?
http://www.aircraftdesign.com/
KENAT, probably the least qualified checker you'll ever meet...