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TANCET 2024
List of top Questions asked in TANCET- 2024
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 combustion in a gas turbine is a
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
In the subcritical operation mode of a supersonic inlet, shock strands
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Hypersonic Air-Breathing Propulsion
Modified Tsai-Hill theory
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Failure theories
Which type of grids is the best for flow over an airfoil?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
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
The deflection of the free end of a cantilever beam subjected to a concentrated load at its mid span is given by:
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Deflection of 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
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Bending
Numerical panel methods are applicable for
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
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
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Composite Materials
The physical principle used for the derivation of momentum equation is
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid flow
The schadowgraph flow visualization technique depends on
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
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?
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
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Air and Gas Compressors
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
What is the Coefficient of pressure, where velocity at the surface of the cylinder is equal to free stream velocity?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
What is the purpose of a fuel injection system in the combustor?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
Pressure gradient in the flow direction
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Heat Transfer
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
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
If there is no change in static enthalpy and static pressure across a rotor, then the turbo-machine is called
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
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
Which of the following is usually measured as the angle between the line of 25% chord and a perpendicular to the root chord?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
When airfoil thickness decreases, the critical Mach number
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
Aerodynamic center is defined as point on the airfoil at which
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
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