Explore topic-wise MCQs in Aerodynamics.

This section includes 7 Mcqs, each offering curated multiple-choice questions to sharpen your Aerodynamics knowledge and support exam preparation. Choose a topic below to get started.

1.

The trends of velocity change in a duct for both subsonic and supersonic flow are identical.

A. True
B. False
Answer» C.
2.

Which equation is obtained when Mach number is equated to zero in area-velocity relation?

A. Momentum equation
B. Continuity equation
C. Energy equation
D. Bernoulli s equation
Answer» C. Energy equation
3.

What is the minimum area of a duct known as?

A. Throat
B. Minimum area duct
C. Convergent duct
D. Divergent duct
Answer» B. Minimum area duct
4.

What happens to the velocity of the supersonic flow in the convergent duct?

A. Decreases
B. Increases
C. Remains the same
D. Changes periodically
Answer» B. Increases
5.

For which of these flows do we need a divergent duct to increase the velocity of the flow?

A. Subsonic flow
B. Supersonic flow
C. Hypersonic flow
D. Sonic flow
Answer» C. Hypersonic flow
6.

For a subsonic flow, what should be the value of dA to get flow acceleration?

A. Zero
B. Negative
C. Positive
D. One
Answer» C. Positive
7.

Sonic flow exists at the throat of an equilibrium chemically reacting nozzle flow?

A. True
B. False
Answer» B. False