Aerospace Engineering
2024 · Paper 1
Take it one question at a time. Try an answer, then check your understanding.
Complete GATE AE 2024 Paper 1 overview, original pages and practice · Timed previous-paper practice
Questions 34–36 of 65. Imported answers require review unless explicitly marked reviewed.
Question 34
Open questionAENAT1 markNeeds review
An aircraft with a turbojet engine is flying with 250 m/s speed at an altitude, where the density of air is 1 kg/m
. The inlet area of the engine is 1 m
. The average velocity of the exhaust gases at the exit of the nozzle, with respect to aircraft, is 550 m/s. Assume the engine exit pressure is equal to the ambient pressure and the fuel-air ratio is negligible. The uninstalled thrust produced by the engine at these conditions is ________ N (rounded off to the nearest integer).Log in to check the answer
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Open questionAENAT1 markNeeds review
Using thin airfoil theory, the lift coefficient of a NACA 0012 airfoil placed at 5° angle of attack in a uniform flow is __________ (rounded off to 2 decimal places).
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Open questionAEMCQ2 marksNeeds review
Given
, where
and
are non-zero real numbers, the value of the differential expression
isYour answerChoose one option.
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