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Span-loading is defined as __________

(a) distribution of weight along span as lift distribution

(b) thrust loading

(c) wing loading

(d) inverse of power loading

I got this question in my homework.

My question comes from Configuration Layout topic in chapter Configuration Layout Considerations of Aircraft Design

1 Answer

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Best answer
Correct option is (a) distribution of weight along span as lift distribution

The best explanation: Span-loading is the distribution of weight along span as lift is distributed. Thrust loading is the ratio of thrust and weight. Wing loading is weight per area. Power loading is weight of aircraft to the power produced.

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