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questions
List of practice Questions
The ratio of modulus of rigidity to bulk modulus for a Poisson's ratio of 0.25 would be:
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Stresses in Beams
The stress due to suddenly applied load is _______ compared to that of the gradually applied load?
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TANCET
Aeronautical and Aerospace Engineering
Stresses and strains
In a short column with eccentric loading, the neutral axis:
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TANCET
Aeronautical and Aerospace Engineering
Columns and Biaxial Stress System
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:
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Stresses in Beams
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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TANCET
Aeronautical and Aerospace Engineering
Deflection of beams
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
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Torsion
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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Aeronautical and Aerospace Engineering
Springs
Modified Tsai-Hill theory
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Aeronautical and Aerospace Engineering
Failure theories
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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TANCET
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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TANCET
Aeronautical and Aerospace Engineering
Composite Materials
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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TANCET
Aeronautical and Aerospace Engineering
Energy methods
Which of the following statements is NOT true of a 1-D problem represented using 2-node line elements as indicated?
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TANCET
Aeronautical and Aerospace Engineering
Finite Element Methods
Which of the following assumptions / statements is NOT true about the Euler-Bernoulli beam theory?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Stresses in Beams
The shape functions indicated here are for a
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Finite Element Methods
Axisymmetric problems involving axisymmetric loading and solids of revolution can be conveniently formulated with the following element type.
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TANCET
Aeronautical and Aerospace Engineering
Finite Element Methods
Which of the following statements is true about Finite Element Analysis (FEA)?
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TANCET
Aeronautical and Aerospace Engineering
Finite Element Methods
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
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Bending
The shear centre position of a thin-walled symmetrical channel section will lie
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TANCET
Aeronautical and Aerospace Engineering
Shear Centre
Shear flow has the same units as
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TANCET
Aeronautical and Aerospace Engineering
Shear Centre
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.
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Stresses in Beams
The physical principle used for the derivation of momentum equation is
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TANCET
Aeronautical and Aerospace Engineering
Fluid flow
The lifting flow over circular cylinder is obtained by the combination of
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TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
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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TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
Winglets are used to reduce
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TANCET
Aeronautical and Aerospace Engineering
Aircraft Configurations
When a nozzle is said to be over expanded?
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TANCET
Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
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