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TANCET
List of top Questions asked in TANCET
A closely coiled helical spring has a stiffness of 8N/mm. If it extends by 5 mm, the energy absorbed is
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Springs
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
Pressure gradient in the flow direction
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Heat Transfer
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
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
Which of the following is a barotropic flow?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
Flow separation is due to
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
Which of the following statements is NOT true of a 1-D problem represented using 2-node line elements as indicated?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Finite Element Methods
In a short column with eccentric loading, the neutral axis:
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Columns and Biaxial Stress System
Numerical panel methods are applicable for
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
Which one of the following is not an example of an adapted nozzle?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Rocket Propulsion
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
TANCET - 2024
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
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Energy 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
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Shear Centre
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
The physical principle used for the derivation of momentum equation is
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid flow
Which of the following statements is true about Finite Element Analysis (FEA)?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Finite Element Methods
Consider an infinitely thin flat plate at an angle of attack of \(5^\circ\) in a Mach 2.3 flow. Pressure is 101 kPa. The lift coefficient as per shock expansion theory is
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Hypersonic Air-Breathing Propulsion
The stress due to suddenly applied load is _______ compared to that of the gradually applied load?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Stresses and strains
For isentropic flows the value of work-done factor for a turbo machine (\(\Psi\)) will be
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
For a flow a Prandtl-Meyer expansion wave is
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
Shear flow has the same units as
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Shear Centre
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
Which of these analyses needs a stretched grid?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
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