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Load factor is defined as _______________

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in Aircraft Design by (701k points)
Load factor is defined as _______________

(a) ratio of lift produced to the weight of aircraft

(b) aerodynamic efficiency

(c) thrust loading

(d) power to weight ratio

I had been asked this question in semester exam.

This intriguing question comes from Air Loads topic in chapter Structures and Loads of Aircraft Design

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Right option is (a) ratio of lift produced to the weight of aircraft

The explanation: Load factor is defined as the ratio of lift produced and the weight of the aircraft. For cruising flight lift is equal to weight. Hence, at such flight condition load factor is unity. Aerodynamic efficiency is defined as ratio of lift to drag. It is directly affected by aerodynamics of the aircraft. Thrust loading is ratio of thrust to weight ratio.

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