This set of Aerodynamics Multiple Choice Questions & Answers (MCQs) focuses on “Area-Velocity Relation”.
1. Sonic flow exists at the throat of an equilibrium chemically reacting nozzle flow?
a) True
b) False
View Answer
Explanation: According to the area-velocity relation for a quasi one-dimensional flow, the relation is given as:
\(\frac {dA}{A}\)=(M2-1)\(\frac {du}{u}\)
For sonic flow, Mach number = 1. Therefore for M=1 we get \(\frac {dA}{A}\)=0, thus sonic flow does exist for an equilibrium reacting nozzle flow at the throat.
2. For a subsonic flow, what should be the value of dA to get flow acceleration?
a) Zero
b) Negative
c) Positive
d) One
View Answer
Explanation: According to the area-velocity relation for a quasi one-dimensional flow, when the flow is subsonic Mach number is less than 1 resulting in the quantity M2-1 being negative. Therefore for achieving accelerated flow, dA has to be negative.
3. 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
View Answer
Explanation: The area-velocity relation is given by:
\(\frac {dA}{A}\)=(M2-1)\(\frac {du}{u}\)
According to this formula, for supersonic flows the value of M2-1 is positive since M > 1. Thus, with increasing cross-sectional area, the velocity increases. Increasing area is achieved by convergent 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
View Answer
Explanation: Since the supersonic flows have Mach number greater than 1, the value of M2-1 is positive. According to the area-velocity relation, for a convergent duct in which dA is negative, the velocity decreases.
5. What is the minimum area of a duct known as?
a) Throat
b) Minimum area duct
c) Convergent duct
d) Divergent duct
View Answer
Explanation: In a nozzle which is designed to achieve supersonic speed, there’s both converging and diverging section which is used to accelerate the flow. There is a minimum area point in the duct where Mach number reaches 1. This minimum area place in a duct is known as the throat.
6. 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
View Answer
Explanation: The area-velocity relation is given by:
\(\frac {dA}{A}\)=(M2-1)\(\frac {du}{u}\)
In the above equation if we substitute M=0 we get,
\(\frac {dA}{A}=-\frac {du}{u}\)
On integrating this equation we get:
Au=constant
This is the continuity equation for incompressible flow in a duct
7. The trends of velocity change in a duct for both subsonic and supersonic flow are identical.
a) True
b) False
View Answer
Explanation: For a flow in a duct, both supersonic and subsonic flows show opposite trends. For a subsonic flow (M < 1), the velocity increases in a convergent duct and decreases in the divergent duct. On the other hand, for a supersonic flow (M > 1), the flow increases in a divergent duct and decreases in the convergent duct.
Sanfoundry Global Education & Learning Series – Aerodynamics.
To practice all areas of Aerodynamics, here is complete set of 1000+ Multiple Choice Questions and Answers.
If you find a mistake in question / option / answer, kindly take a screenshot and email to [email protected]
- Check Aerodynamics Books
- Check Aerospace Engineering Books
- Check Aeronautical Engineering Books
- Apply for Aerospace Engineering Internship
- Practice Aerospace Engineering MCQs
