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Aerodynamics Practice Test: Basic Compressible Flow
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Basic Compressible Flow topics include: Thermodynamics, compressibility and stagnation conditions. Compressible flow is a branch of fluid mechanics that studies flows with significant changes in fluid density. In compressible flows, the fluid density and pressure depend on the velocity magnitude relative to the speed of sound in the fluid.  Compressible flows are usually high-speed flows with Mach numbers greater than about 0.3. Examples of compressible flow include: Flow over a wing or aircraft nacelle Flow through high-performance valves  Compressible fluid flow is different from... Show more
Aerodynamics Practice Test: Basic Compressible Flow
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25 Questions

1. Which is the wrong result for a calorically perfect gas?
2. The incorrect formula for entropy for a calorically perfect gas is____
3. The total pressure and total density are present there only for an isentropic flow.
4. For a steady, inviscid, adiabatic flow of a gas, the total temperate is constant along the flow.
5. The incorrect formula for the specific heat of an ideal gas in terms of specific heat ratio of a gas and universal gas constant is_____
6. The equation of state for a perfect gas is p = δRT, where R is______ (for air at standard conditions).
7. An isentropic process is restrictive and is not feasible in real life.
8. In physical sense, compressibility is the fractional change in volume of the fluid element per unit change in_____
9. Flow over a rocket outside the boundary layer is isentropic.
10. The first law of thermodynamics is proved by experiments. Select the correct choice for it.
11. For a block of ice on a plate, second law of thermodynamics says that____
12. The best estimate of whether the flow is compressible or not comes from ______
13. Identify the incorrect source for the corresponding variables of the first law.
14. Mach number is defined as the ratio of local flow velocity to the _______
15. Which of these is not an assumption made when we derive the equation h + V2/2 = constant?
16. The constant h + V2/2 for an inviscid, adiabatic and a steady flow is equal to the stagnation enthalpy for the fluid.
17. Which is the correct result according to the second law of thermodynamics?
18. For the flow over an airfoil, which of the following is the incorrect statement if the fluid is liquid?
19. The isothermal compressibility for a gas is same as isothermal compressibility.
20. The stagnation pressure can be visualized as the pressure we feel when we ride along the gas molecules at the local flow velocity.
21. The pressure which is a result of the random motion of the gas molecules is ______
22. Select the incompressible flow out of the following.
23. For a reversible process, which is not the correct statement?
24. τT and τS are precise thermodynamic properties of the gas and the values can be obtained easily.
25. Specific heat for gas is almost constant in the case of_______