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Aeronautical and Aerospace Engineering
List of top Aeronautical and Aerospace Engineering Questions
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
The lifting flow over circular cylinder is obtained by the combination of
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Aeronautical and Aerospace Engineering
Airfoil Theory
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
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Aeronautical and Aerospace Engineering
Air and Gas Compressors
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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Aeronautical and Aerospace Engineering
Airfoil Theory
The schadowgraph flow visualization technique depends on
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Aeronautical and Aerospace Engineering
Airfoil Theory
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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Aeronautical and Aerospace Engineering
Deflection of beams
Flow separation is due to
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Aeronautical and Aerospace Engineering
Airfoil Theory
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?
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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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Aeronautical and Aerospace Engineering
Energy methods
Aerodynamic center is defined as point on the airfoil at which
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Aeronautical and Aerospace Engineering
Airfoil Theory
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
Modified Tsai-Hill theory
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Aeronautical and Aerospace Engineering
Failure theories
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 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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Aeronautical and Aerospace Engineering
Aircraft Configurations
The physical principle used for the derivation of momentum equation is
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Aeronautical and Aerospace Engineering
Fluid flow
When a nozzle is said to be over expanded?
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Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
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
Which of the following is a barotropic flow?
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Aeronautical and Aerospace Engineering
Fundamentals of Supersonic Flows
Shear flow has the same units as
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Aeronautical and Aerospace Engineering
Shear Centre
For calorically perfect gas, specific heats \(C_p\) and \(C_v\) are
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Aeronautical and Aerospace Engineering
Heat Transfer
Pressure gradient in the flow direction
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Aeronautical and Aerospace Engineering
Heat Transfer
When airfoil thickness decreases, the critical Mach number
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Aeronautical and Aerospace Engineering
Airfoil Theory
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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Aeronautical and Aerospace Engineering
Springs
What is the purpose of supercritical airfoil?
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Aeronautical and Aerospace Engineering
Airfoil Theory
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