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Aerospace Engineering
List of top Aerospace Engineering Questions asked in TS PGECET
The main thermodynamic cycle used in a turbojet engine is
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Aircraft Engines
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
A convergent-divergent nozzle is used in jet engines to
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
In a ramjet engine, the air compression takes place by
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
In a jet engine's combustion chamber, detonation refers to
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
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 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
Let \(A\) be a square matrix. Which of the following statement about eigenvectors is correct?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Structural Dynamics
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
In the context of mechanical vibrations, static coupling refers to
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 standard shear flow formula \[ q=\frac{VQ}{I} \] is not applicable to thick-walled sections. The primary reason is
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Flight vehicle structures
A symmetrical section subjected to a load inclined to its principal axis will produce
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Strength of Materials
Which structural design philosophy allows the outer skin of an aircraft to carry a significant portion of the load?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Flight vehicle structures
According to Bredt--Batho theory, shear flow in a thin-walled closed section under torsion is
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Flight vehicle structures
For a thin-walled C-channel, why does a load applied at the centroid produce twisting?
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Flight vehicle structures
On a principal plane, the relationship between the stress components is such that
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Strength of Materials
According to Rankine's failure theory, failure occurs when
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Strength of Materials
A plane truss has \(10\) joints. For it to be a perfect truss, the number of members must be
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Flight vehicle structures
According to Tresca theory, yielding begins when
TS PGECET - 2026
TS PGECET
Aerospace Engineering
Strength of Materials
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