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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
Potential function for three dimensional doublet of strength \( \mu \) is
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid flow
For a given rotational speed of a rotor of an axial flow compressor, as the fan tip radius increases, the centrifugal stress on the fan blade
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Aeronautical and Aerospace Engineering
Air and Gas Compressors
Which of the following states that the time rate of change of circulation around a closed curve consisting of the same fluid elements is zero?
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Aeronautical and Aerospace Engineering
Fluid flow
AB = 40 cm while BC = 30 cm. Areas A and C are equal to 8 \( \text{cm}^2 \) while areas B and D are 6 \( \text{cm}^2 \). The given section is subject to \( M_x = 100 \text{kNm} \) and \( M_y = 40 \text{kNm} \). Find an expression for the bending stress. Assume that the webs are ineffective in bending.
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Aeronautical and Aerospace Engineering
Stresses in Beams
The physical principle used for the derivation of momentum equation is
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Aeronautical and Aerospace Engineering
Fluid flow
If two shafts of same length, one of which is hollow, transmit equal torque and have equal maximum shear stress, then they should have equal
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Aeronautical and Aerospace Engineering
Torsion
A rectangular section beam subjected to a bending moment M varying along its length is required to develop the same maximum bending stress at any cross section. If the depth of the section is constant, then its width will vary as:
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Aeronautical and Aerospace Engineering
Stresses in Beams
Shear flow has the same units as
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Aeronautical and Aerospace Engineering
Shear Centre
The function \( y = A \left(1 - \cos\left(\frac{2\pi x}{L}\right)\right) \) is an allowed approximate function for a
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Aeronautical and Aerospace Engineering
Energy methods
If a laminate consists of pairs of layers with identical thickness and elastic properties, but with orientation of +θ and -θ with respect to the laminate reference axis, then the laminate is called as
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Aeronautical and Aerospace Engineering
Composite Materials
The Shear stresses in the fiber and matrix are 200GPa and 20GPa respectively. If the fiber volume fraction is 70%, then the longitudinal compressive strength of the lamina is
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Aeronautical and Aerospace Engineering
Composite Materials
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
Which type of grids is the best for flow over an airfoil?
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Aeronautical and Aerospace Engineering
Fluid Dynamics
Modified Tsai-Hill theory
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Aeronautical and Aerospace Engineering
Failure theories
The shear centre position of a thin-walled symmetrical channel section will lie
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Aeronautical and Aerospace Engineering
Shear Centre
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
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
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
Ram efficiency is defined as
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Aeronautical and Aerospace Engineering
Heat Transfer
In a short column with eccentric loading, the neutral axis:
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Aeronautical and Aerospace Engineering
Columns and Biaxial Stress System
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
Which of these analyses needs a stretched grid?
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Aeronautical and Aerospace Engineering
Fluid Dynamics
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
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