1.) a.) When flying at the highest, negative angle of attack (-HAA), the largest compressive stress in a wing will be on

[answerhappygod]

1.)
a.) When flying at the highest, negative angle of attack (-HAA),
the largest compressive stress in a wing will be on the upper,
leading edge spar cap, while the largest tensile stress will be on
the lower, trailing edge spar cap. TRUE OR
FALSE?
b.) When flying at the lowest, positive angle of
attack (+LAA), the largest compressive stress in a wing will be on
the upper, trailing edge spar cap while the largest tensile stress
will be on the lower, leading edge spar cap. TRUE OR
FALSE?