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Which of the following is correct? (a)W0 = N*T per engine / Thrust loading

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Which of the following is correct?

(a) W0 = N*T per engine / Thrust loading

(b) W0 = Number of engine

(c) W0 = T per engine / Thrust loading

(d) W0 = 1 / Thrust loading

I had been asked this question during an interview.

This question is from Fixed-Engine Sizing in portion Initial Sizing of Aircraft Design

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Right answer is (a) W0 = N*T per engine / Thrust loading

The best explanation: For fixed engine sizing if we allow range to vary then, we can simply estimate take-off gross weight as W0 = N*T per engine / Thrust loading. Here, N is the total number of engine of an aircraft.

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