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Aerospace Engineering
List of top Aerospace Engineering Questions asked in TS PGECET
The primary function of the inducer in a centrifugal compressor is to
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Centrifugal Compressors
The work done per unit mass in a centrifugal compressor mainly depends on
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Centrifugal Compressors
Slip factor in a centrifugal compressor accounts for
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Centrifugal Compressors
In an impulse turbine stage (degree of reaction \(=0\))
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Axial Turbines
The degree of reaction in an axial compressor stage is
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Axial Compressors
An axial turbine stage has a degree of reaction of \(50\%\) and operates with symmetrical velocity triangles (i.e., absolute inlet and exit flow angles are equal in magnitude but opposite in direction). The axial velocity remains constant through the stage. Which of the following statements is correct?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Axial Turbines
Stage efficiency of a single-stage axial compressor is defined as
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Axial Compressors
A convergent-divergent nozzle is used in jet engines to
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Aircraft Engines
The work done by the rotor in an axial compressor primarily results in
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Axial Compressors
In an axial compressor, the change in angular momentum of air through the rotor is directly related to
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Axial Compressors
The main thermodynamic cycle used in a turbojet engine is
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Aircraft Engines
Which of the following sequences correctly represents the flow of air in a basic turbojet engine?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Aircraft Engines
The degree of reaction of an axial compressor stage is defined as the ratio of
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Axial Compressors
In a ramjet engine, the air compression takes place by
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Aircraft Engines
A turbofan engine has a high bypass ratio, meaning most of the air flows through the bypass duct instead of the core. The engine manufacturer claims this design "improves fuel efficiency and reduces noise". Which of the following statements reflects the best critical evaluation of this claim?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Aircraft Engines
Which of the following statement about Airy's stress function \(\phi(x,y)\) is correct?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Strength of Materials
In the context of mechanical vibrations, static coupling refers to
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Structural Dynamics
In a jet engine's combustion chamber, detonation refers to
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Aircraft Engines
A man is sitting inside a house during the winter season. The main mode of heat transfer from the man's body to the surroundings is
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Fluid Mechanics
Let \(A\) be a square matrix. Which of the following statement about eigenvectors is correct?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Structural Dynamics
In an under damped single degree of freedom system, the ratio of the first peak amplitude to the seventh peak amplitude is \[ \frac{x_1}{x_7}=64. \] Then, the ratio of two successive peak amplitudes is
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Structural Dynamics
Which specific flight load acts like a 'hammer blow' to the wing structure, momentarily increasing the angle of attack and lift?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Flight vehicle structures
Which material property is most important for the web of a Wagner Beam?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Flight vehicle structures
In a Semi-Monocoque wing undergoing upward bending, which of the following is true regarding the wing skins?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Flight vehicle structures
The natural frequency of a simple spring-mass system with static deflection \(9.81\ \text{cm}\) is
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Structural Dynamics
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