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Aerodynamics Practice Test: Inviscid & Incompressible Flow
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Inviscid & Incompressible Flow topics include: Bernoulli’s equation, duct incompressible flow, pitot tube, pressure coefficient, uniform, source and doublet flows, nonlifting flow over cylinder and arbitrary bodies, lifting flow over cylinder, kutta joukowski theorem and vortex flow. Inviscid flow is a theoretical concept in fluid dynamics that describes the flow of a fluid with zero viscosity. Some key features of inviscid flow include: No energy is lost due to internal friction The flow is reversible No wake is formed behind a body placed in an inviscid flow Boundary layers are absent... Show more
Aerodynamics Practice Test: Inviscid & Incompressible Flow
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25 Questions

1. Incompressible flow is the one in which density is ___________
2. If the value of Cp=1, then the local pressure can be given as ___________
3. What are the quantitative flow visualization techniques?
4. The pressure measured relative to vacuum is ______
5. When the velocity at a point becomes zero, it refers to ___________
6. ___________ is the scalar function of the space and time.
7. What will be the shape of Rankine oval when U*y+ ((-u/2*pi*r) = 0?
8. The flow past cylinder is also called as _________
9. What will be the shape of Rankine oval when sin θ=0?
10. Which of the following is an application of incompressible flow in a duct?
11. Density is ratio of __________
12. The opposite case of the source flow is ___________
13. Consider a flow over a flat plate of uniform cross section area, the flow moves at a constant speed. Due to a certain disturbance, there is a disturbance in the flow. In the given scenario, which of the following statement is true?
14. Which of the following parameter can be measured using venturi?
15. An increase in the speed of the flow leads to an increase in kinetic energy and dynamic pressure.
16. When the local flow velocity is zero itself then _________
17. Bernoulli’s equation is applicable only for _______
18. The following figure is an example of ____________
Find the type of flow of streamlines in concentric circles in the given figure
19. When the amount of fluid displaced is equal to weight of body, it is called as _______
20. What is passive flow control method used to reduce the drag co-efficient over a cylinder?
21. The dynamic pressure is given by ______
22. The dynamic pressure can be used in all flows from incompressible to hypersonic.
23. The strength of the vortex flow can be given by ______________
24. In a wind tunnel, the section with minimum area is called as __________
25. The dynamic pressure can be given by ____________