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Tamil Nadu Common Entrance Test
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Aeronautical and Aerospace Engineering
List of top Aeronautical and Aerospace Engineering Questions asked in Tamil Nadu Common Entrance Test
Axisymmetric problems involving axisymmetric loading and solids of revolution can be conveniently formulated with the following element type.
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Finite Element Methods
Which of the following is usually measured as the angle between the line of 25% chord and a perpendicular to the root chord?
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Aeronautical and Aerospace Engineering
Airfoil Theory
The stress due to suddenly applied load is _______ compared to that of the gradually applied load?
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Aeronautical and Aerospace Engineering
Stresses and strains
Flow separation is due to
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Aeronautical and Aerospace Engineering
Airfoil Theory
Which type of grids is the best for flow over an airfoil?
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Aeronautical and Aerospace Engineering
Fluid Dynamics
Aerodynamic center is defined as point on the airfoil at which
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Aeronautical and Aerospace Engineering
Airfoil Theory
Which of the following statements is true about Finite Element Analysis (FEA)?
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Aeronautical and Aerospace Engineering
Finite Element Methods
The free stream Mach number for which the entire flow around the body is subsonic is called
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Aeronautical and Aerospace Engineering
Airfoil Theory
The shear centre position of a thin-walled symmetrical channel section will lie
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Aeronautical and Aerospace Engineering
Shear Centre
What is the purpose of supercritical airfoil?
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Aeronautical and Aerospace Engineering
Airfoil Theory
The ratio of modulus of rigidity to bulk modulus for a Poisson's ratio of 0.25 would be:
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Aeronautical and Aerospace Engineering
Stresses in Beams
The semi-span of a rectangular wing of plan form area 8.4 m² is 3.5 m. The aspect ratio of the wing is
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Aeronautical and Aerospace Engineering
Aircraft Configurations
Consider an equal-leg angle section cantilever beam subject to a vertical shearing load at the tip where the line of action of the applied vertical force passes through the centroid. This beam will experience
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Aeronautical and Aerospace Engineering
Bending
For which of these applications is the turbo shaft engine most suited?
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Aeronautical and Aerospace Engineering
Aircraft Configurations
Which of the following assumptions / statements is NOT true about the Euler-Bernoulli beam theory?
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Aeronautical and Aerospace Engineering
Stresses in Beams
When a nozzle is said to be over expanded?
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Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
Ram efficiency is defined as
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Aeronautical and Aerospace Engineering
Heat Transfer
Which of the following is a barotropic flow?
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Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
In a short column with eccentric loading, the neutral axis:
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Aeronautical and Aerospace Engineering
Columns and Biaxial Stress System
In the subcritical operation mode of a supersonic inlet, shock strands
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Aeronautical and Aerospace Engineering
Hypersonic Air-Breathing Propulsion
The deflection of the free end of a cantilever beam subjected to a concentrated load at its mid span is given by:
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Aeronautical and Aerospace Engineering
Deflection of beams
For calorically perfect gas, specific heats \(C_p\) and \(C_v\) are
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Aeronautical and Aerospace Engineering
Heat Transfer
Pressure gradient in the flow direction
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Aeronautical and Aerospace Engineering
Heat Transfer
Numerical panel methods are applicable for
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Aeronautical and Aerospace Engineering
Fluid Dynamics
A closely coiled helical spring has a stiffness of 8N/mm. If it extends by 5 mm, the energy absorbed is
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TANCET
Aeronautical and Aerospace Engineering
Springs
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