Question 31

AENAT1 markNeeds review
An aircraft starts gliding in power-off condition at an altitude of 4 km. Given that the maximum lift to drag ratio of the aircraft is 15, the maximum glide range that the aircraft can cover, measured along the ground, is ________ km (rounded off to the nearest integer).

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2026AE

GATE AE 2026 · Paper 1

Aerospace Engineering · Original paper archive

Section
Aerospace Engineering
Question type
Numerical answer (NAT)
Marks
1 mark

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