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Tamil Nadu Common Entrance Test
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Aeronautical and Aerospace Engineering
List of top Aeronautical and Aerospace Engineering Questions asked in Tamil Nadu Common Entrance Test
The critical mass flow rate through a converging-diverging nozzle
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Aeronautical and Aerospace Engineering
Gas Turbines
What is the Coefficient of pressure, where velocity at the surface of the cylinder is equal to free stream velocity?
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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?
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Aeronautical and Aerospace Engineering
Fluid flow
When airfoil thickness decreases, the critical Mach number
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Aeronautical and Aerospace Engineering
Airfoil Theory
What is the purpose of supercritical airfoil?
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Aeronautical and Aerospace Engineering
Airfoil Theory
A turbojet powered aircraft is suitable for which of the following type of applications?
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Aeronautical and Aerospace Engineering
Aircraft Configurations
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
For calorically perfect gas, specific heats \(C_p\) and \(C_v\) are
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Aeronautical and Aerospace Engineering
Heat Transfer
The schadowgraph flow visualization technique depends on
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Aeronautical and Aerospace Engineering
Airfoil Theory
Flow separation is due to
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Aeronautical and Aerospace Engineering
Airfoil Theory
Aerodynamic center is defined as point on the airfoil at which
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Aeronautical and Aerospace Engineering
Airfoil Theory
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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Aeronautical and Aerospace Engineering
Hypersonic Air-Breathing Propulsion
Winglets are used to reduce
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Aeronautical and Aerospace Engineering
Aircraft Configurations
When a nozzle is said to be over expanded?
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Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
For a flow a Prandtl-Meyer expansion wave is
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Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
Which of the following is a barotropic flow?
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Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
The lifting flow over circular cylinder is obtained by the combination of
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Aeronautical and Aerospace Engineering
Airfoil Theory
The physical principle used for the derivation of momentum equation is
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Aeronautical and Aerospace Engineering
Fluid flow
The shear centre position of a thin-walled symmetrical channel section will lie
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Aeronautical and Aerospace Engineering
Shear Centre
Potential function for three dimensional doublet of strength \( \mu \) is
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Aeronautical and Aerospace Engineering
Fluid flow
Shear flow has the same units as
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Aeronautical and Aerospace Engineering
Shear Centre
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
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Aeronautical and Aerospace Engineering
Bending
Which of the following statements is true about Finite Element Analysis (FEA)?
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Aeronautical and Aerospace Engineering
Finite Element Methods
Which of the following assumptions / statements is NOT true about the Euler-Bernoulli beam theory?
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Aeronautical and Aerospace Engineering
Stresses in Beams
Which of the following statements is NOT true of a 1-D problem represented using 2-node line elements as indicated?
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Aeronautical and Aerospace Engineering
Finite Element Methods
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