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Last Updated On [03-11-2023]

In a semi-monocoque construction of an aircraft wing, the skin and spar webs are the primary carriers of
(A) shear stresses due to an aerodynamic moment component alone.
(B) normal (bending) stresses due to aerodynamic forces.
(C) shear stresses due to aerodynamic forces alone.
(D) shear stresses due to aerodynamic forces and a moment component.


Question ID - 156229 :-

In a semi-monocoque construction of an aircraft wing, the skin and spar webs are the primary carriers of
(A) shear stresses due to an aerodynamic moment component alone.
(B) normal (bending) stresses due to aerodynamic forces.
(C) shear stresses due to aerodynamic forces alone.
(D) shear stresses due to aerodynamic forces and a moment component.

1 Answer
5876 Votes
3537

Answer Key : (D) -

(D) shear stresses due to aerodynamic forces and a moment component.



Next Question :

The logarithmic decrement measured for a viscously damped single degree of freedom system is 0.125. The value of the damping factor in $\%$ is closest to
(A) 0.5
(B) 1.0
(C) 1.5
(D) 2.0


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