Complete GATE AE 2023 Paper 1 overview, original pages and practice · Timed previous-paper practice

Questions 37–39 of 65. Imported answers require review unless explicitly marked reviewed.

Paper practice 65 questionsPage 13 of 22

Question 37

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A supersonic aircraft has an air intake ramp that can be rotated about the leading edge O such that the shock from the leading edge meets the cowl lip as shown in the figure. Select all the correct statement(s) as per oblique shock theory when the flight Mach number M is increased.
Diagram for Aerospace Engineering question 37

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Question 38

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Two missiles A and B powered by solid rocket motors have identical specific impulse, liftoff mass of 560 kg each, and burn durations of

s and

s, respectively. The propellant mass flow rates,

and

, for missiles A and B, respectively, are given by


Neglecting gravity and aerodynamic forces, the relationship between the final velocities

and

of missiles A and B, respectively, is given by
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Question 39

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A perfect gas stored in a large reservoir exhausts into the atmosphere through a convergent duct. The reservoir pressure is

and temperature is

. The jet emerges from the nozzle at choked conditions with average velocity

, Mach number M, pressure p, temperature T, and density

. If the reservoir pressure is increased, then
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