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Tamil Nadu Common Entrance Test
List of top Questions asked in Tamil Nadu Common Entrance Test
When a nozzle is said to be over expanded?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
Shear flow has the same units as
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TANCET
Aeronautical and Aerospace Engineering
Shear Centre
For which of these applications is the turbo shaft engine most suited?
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TANCET
Aeronautical and Aerospace Engineering
Aircraft Configurations
When airfoil thickness decreases, the critical Mach number
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TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
Specific impulse of a rocket
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TANCET
Aeronautical and Aerospace Engineering
Rocket Propulsion
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
What is the purpose of a fuel injection system in the combustor?
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TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
What is the center pressure if the lift coefficient and lift curve slope of an aerofoil of percentage camber 0.6 are 1.02 and 2, respectively?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
The combustion in a gas turbine is a
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TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
The concept of erosive burning in solid rocket propellant operation pertains to
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TANCET
Aeronautical and Aerospace Engineering
Rocket Propulsion
The critical mass flow rate through a converging-diverging nozzle
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TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
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
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 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
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 laminar flame speed in a combustion chamber of a jet engine is
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TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
The lifting flow over circular cylinder is obtained by the combination of
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TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
A turbojet powered aircraft is suitable for which of the following type of applications?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Aircraft Configurations
Characteristic velocity of a rocket engine is equal to
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Rocket Propulsion
If there is no change in static enthalpy and static pressure across a rotor, then the turbo-machine is called
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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
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TANCET
Aeronautical and Aerospace Engineering
Springs
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
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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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 ratio of modulus of rigidity to bulk modulus for a Poisson's ratio of 0.25 would be:
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TANCET
Aeronautical and Aerospace Engineering
Stresses in Beams
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