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The range factor is proportional to the square root of the initial cruising weight.

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in Aircraft Performance by (558k points)
The range factor is proportional to the square root of the initial cruising weight.

(a) True

(b) False

The question was posed to me in unit test.

This key question is from Effect of WAT on Cruise Performance in section Cruising Performance of Aircraft Performance

1 Answer

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Best answer
Correct choice is (a) True

The explanation is: The range factor is proportional to the square root of the initial cruising weight. This way we know that the range of the aircraft will increase with its weight. This implies that increase in weight increases the fuel availability for the cruise.

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