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questions
List of practice Questions
What is the purpose of a fuel injection system in the combustor?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
The critical mass flow rate through a converging-diverging nozzle
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
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
Pressure gradient in the flow direction
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Heat Transfer
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
In a turbojet engine, thrust specific fuel consumption ________ with increasing compressor pressure ratio and __________ with increasing turbine inlet temperature (within range of operation).
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
Specific impulse of a rocket
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Rocket Propulsion
The concept of erosive burning in solid rocket propellant operation pertains to
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Rocket Propulsion
Which one of the following is not an example of an adapted nozzle?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Rocket Propulsion
The laminar flame speed in a combustion chamber of a jet engine is
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Gas Turbines
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
Which of these analyses needs a stretched grid?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
Numerical panel methods are applicable for
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
Which type of grids is the best for flow over an airfoil?
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
The resultant of two forces \( P \) and \( Q \) (such that \( P>Q \)) acting along the same straight line, but in opposite direction, is given by:
TANCET - 2024
TANCET
Automobile Engineering
Mechanics
Mass moment of inertia of a thin rod about its one end is ________ the mass moment of inertia of the same rod about its mid-point.
TANCET - 2024
TANCET
Automobile Engineering
Mechanics
The ratio of static friction to dynamic friction is always:
TANCET - 2024
TANCET
Automobile Engineering
Mechanics
Which one of the following is an open pair?
TANCET - 2024
TANCET
Automobile Engineering
Mechanics
The train value of a gear train is:
TANCET - 2024
TANCET
Automobile Engineering
Automobile Design
A porter governor is a______ governor.
TANCET - 2024
TANCET
Automobile Engineering
Automobile Design
Consider the following statements about theory of simple bending:
(i) Beam material is isotropic and homogeneous
(ii) Elastic modulus of beam material is more in tension than in compression
(iii) Radius of curvature is large
Of these statements,
TANCET - 2024
TANCET
Automobile Engineering
Strength of Materials
If the diameter of a shaft is subjected to torque alone is doubled, then the horse power can be increased to:
TANCET - 2024
TANCET
Automobile Engineering
Strength of Materials
A higher value of flexural rigidity indicates:
TANCET - 2024
TANCET
Automobile Engineering
Strength of Materials
Match list I with list II and select the correct answer using the code given:
TANCET - 2024
TANCET
Automobile Engineering
Automobile Design
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