Aerospace Engineering
GATE AE kind:question PYQs
Build your understanding with focused practice from past exam papers.
Questions 411–420 of 650. Imported answers require independent review unless marked reviewed.
Question 11
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For hyperbolic trajectory of a satellite of mass
having velocity
at a distance
from the center of earth (
: gravitational constant,
: mass of earth), which one of the following relations is true?Your answerChoose one option.
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For conventional airplanes, which one of the following is true regarding roll control derivative
and yaw control derivative
, where
is rudder deflection?Your answerChoose one option.
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The ratio of exit stagnation pressure to inlet stagnation pressure across the rotating impeller of a centrifugal compressor, operating with a closed exit, is
Your answerChoose one option.
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Which one of the following is a hypergolic propellant combination used in rocket engines?
Your answerChoose one option.
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In aircraft engine thermodynamic cycle analysis, perfectly expanded flow in the nozzle means that the static pressure in the flow at the nozzle exit is equal to
Your answerChoose one option.
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Three long and slender aluminum bars of identical length are subjected to an axial tensile force. These bars have circular, triangular and rectangular cross sections, with same cross sectional area. If they yield at
,
and
, respectively, which one of the following is true?Your answerChoose one option.
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The positive high angle-of-attack condition is obtained in a steady pull-out maneuver at the largest permissible angle-of-attack of the wing. Under this condition, at which of the following regions of the wing does the maximum tension occur?

Your answerChoose one option.
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The natural frequency of the first mode of a rectangular cross section cantilever aluminum beam is
rad/s. If the material and cross-section remain the same, but the length of the beam is doubled, the first mode frequency will becomeYour answerChoose one option.
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Given
, the sum of squares of eigenvalues of
isYour answerChoose one option.
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Burnout velocity of a space vehicle in circular orbit at an angle 5 degrees above the local horizon around earth is 13.5 km/s. Tangential velocity of the space vehicle in the orbit is ______ km/s (round off to two decimal places).
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