Explore topic-wise MCQs in Aerodynamics.

This section includes 8 Mcqs, each offering curated multiple-choice questions to sharpen your Aerodynamics knowledge and support exam preparation. Choose a topic below to get started.

1.

For which range of values is the hypersonic similarity rule valid for very slender bodies?

A. K = 0.5 to infinity
B. K > 1.5
C. 0.5 < K < 1.5
D. 2 < K < 1000
Answer» B. K > 1.5
2.

Hypersonic similarity is applicable for only irrotational flow.

A. True
B. False
Answer» C.
3.

On which of this parameter is the coefficient of lift over a two dimensional body at hypersonic flow dependent?

A. . ( frac { }{ } )
B. , K, M<sub> </sub>
C. M<sub> </sub>T, ( frac { }{ } ),
D. M<sub> </sub>T, K,
Answer» D. M<sub> </sub>T, K,
4.

The ratio ( frac {C_p}{ ^{2}} ) behind a shock wave is a function of which of these parameters?

A. Hypersonic similarity parameter K and
B. Angle of attack and wedge angle
C. Coefficient of lift and wedge angle
D. Hypersonic similarity parameter and angle of attack
Answer» B. Angle of attack and wedge angle
5.

Two bodies holding hypersonic similarity at small angle of attack need the values of and M to be same.

A. True
B. False
Answer» C.
6.

For two bodies with same shape but different scales, which of these parameters must be equal for the flow to be same in hypersonic regime?

A. Mach number
B. Product of Mach number and slenderness ratio
C. Tangential flow velocity
D. Normal flow velocity
Answer» C. Tangential flow velocity
7.

Why is hypersonic similarity parameter essential?

A. Supersonic flow over wedges
B. Hypersonic flow over slender bodies
C. Hypersonic flow over cone
D. Hypersonic flow over flat plate
Answer» C. Hypersonic flow over cone
8.

Which of these does not result in two or more flows being dynamically similar?

A. Streamlines are geometrically similar
B. The shape of the blunt body is same
C. Length of the body is same
D. Non dimensional parameters remain same
Answer» D. Non dimensional parameters remain same