POF – 03 Basic Aerodynamic Theory

 

Q1. Bernoulli’s’ theorem indicates that:

A

Q2. Bernoulli’s Theorem states:

B

Q3. The expression, “In a streamlined flow of fluid, the sum of all energies is a constant,” derives from:

B

Q4. Bernoulli’s equation can be written as: (pt = total pressure, ps = static pressure and q = dynamic pressure)

D

Q5. Bernoulli’s equation can be written as (pt = total pressure, ps =static pressure, q = dynamic pressure):

B

Q6. Which one of the following statements about Bernoulli’s theorem is correct?

D

Q7. Bernoulli’s equation is (note: rho is density; pstat is static pressure; pdyn is dynamic pressure; ptot is total pressure)

D

Q8. In a stationary subsonic streamline flow pattern, if the streamlines converge, in this part of the pattern, the static pressure will (i) and the velocity will (ii):

A

Q9. The continuity equation states: If the area of a tube is increasing, the speed of the subsonic and incompressible flow inside is:

D

Q10. Assuming subsonic incompressible flow, how will air density change as air flows through a tube of increasing cross-sectional area?

B

Q11. In a two-dimensional flow pattern, where the streamlines converge the static pressure will:

B

Q12. If in a two-dimensional incompressible and subsonic flow, the streamlines converge the static pressure in the flow will:

C

Q13. Consider a certain stream line tube. The velocity of the stream in the tube is V. An increase of temperature of the stream at constant value of V will:

D

Q14. If the continuity equation is applicable, what will happen to the air density (rho) if the cross sectional area of a tube changes? (low speed, subsonic and incompressible flow):

D

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