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Tamil Nadu Common Entrance Test
List of top Questions asked in Tamil Nadu Common Entrance Test
When airfoil thickness decreases, the critical Mach number
TANCET - 2024
TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
The schadowgraph flow visualization technique depends on
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TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
The semi-span of a rectangular wing of plan form area 8.4 m² is 3.5 m. The aspect ratio of the wing is
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TANCET
Aeronautical and Aerospace Engineering
Aircraft Configurations
In a short column with eccentric loading, the neutral axis:
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TANCET
Aeronautical and Aerospace Engineering
Columns and Biaxial Stress System
The shape functions indicated here are for a
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TANCET
Aeronautical and Aerospace Engineering
Finite Element Methods
The shear centre position of a thin-walled symmetrical channel section will lie
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TANCET
Aeronautical and Aerospace Engineering
Shear Centre
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
In a turbojet engine, thrust specific fuel consumption ________ with increasing compressor pressure ratio and __________ with increasing turbine inlet temperature (within range of operation).
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TANCET
Aeronautical and Aerospace Engineering
Aircraft Configurations
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
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
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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?
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TANCET
Aeronautical and Aerospace Engineering
Stresses and strains
Aerodynamic center is defined as point on the airfoil at which
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TANCET
Aeronautical and Aerospace Engineering
Airfoil Theory
When a nozzle is said to be over expanded?
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TANCET
Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
Winglets are used to reduce
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TANCET
Aeronautical and Aerospace Engineering
Aircraft Configurations
Which type of grids is the best for flow over an airfoil?
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TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
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
Which one of the following is not an example of an adapted nozzle?
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TANCET
Aeronautical and Aerospace Engineering
Rocket Propulsion
Which of these analyses needs a stretched grid?
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TANCET
Aeronautical and Aerospace Engineering
Fluid Dynamics
In the subcritical operation mode of a supersonic inlet, shock strands
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TANCET
Aeronautical and Aerospace Engineering
Hypersonic Air-Breathing Propulsion
A porter governor is a______ governor.
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TANCET
Automobile Engineering
Automobile Design
In which of the following welding methods is the Heat affected zone (HAZ) minimum?
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TANCET
Automobile Engineering
Production Technology
Increasing a proportional gain will:
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TANCET
Automobile Engineering
Automotive Electrical and Electronics
Janney transmission is working as per _________ principle.
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TANCET
Automobile Engineering
Automotive Transmission
Which of the following is the longitudinal framing of the roof at the joining?
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TANCET
Automobile Engineering
Vehicle Body Engineering
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
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