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Design lift coefficient is determined by wing loading.

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in Aircraft Design by (701k points)
Design lift coefficient is determined by wing loading.

(a) True

(b) False

This question was addressed to me in an online interview.

I'm obligated to ask this question of Wing Loading in chapter Thrust-Weight Ratio and Wing Loading of Aircraft Design

1 Answer

+1 vote
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Best answer
The correct choice is (a) True

The best explanation: Wing loading will affect the drag of aircraft. Wing loading directly affects the wetted area and span of the wing. Hence, based on adequate wing loading we can determine lift co-efficient as well.

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