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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. Is Kutta-Joukowski theorem is fundamental theorem of aerodynamics?
2. The shape of the wing is called as ____________
3. Except at the origin where r=0, the vortex flow is ___________
4. In a wing, the coefficient of pressure at the upper surface is greater than the lower surface.
5. What are the quantitative flow visualization techniques?
6. The dynamic pressure is given by ______
7. The flows in which all the flow parameters are the function of ‘x’ is called as _________
8. When both the source and sink are of equal strength it is called ________
9. The dynamic pressure can be used in all flows from incompressible to hypersonic.
10. What types of visualization is used to delay the separation of the flow?
11. Bernoulli’s equation can be applied to compressible flow at which of the following matches the number?
12. The strength of the vortex flow can be given by ______________
13. The following figure is an example of ____________
Find the type of flow of streamlines in concentric circles in the given figure
14. The aircraft fly based on which principle _________
15. The flow in which streamlines are directed away from the origin is called as __________
16. ______ gives the velocity component at right angles to a particular direction.
17. When velocity potential (Φ) is constant, it is called as _________
18. Which of the following parameter can be measured using venturi?
19. When the local flow velocity is zero itself then _________
20. In a pitot tube, the kinetic energy is converted into _________
21. What will be the shape of Rankine oval when sin θ=0?
22. When an aircraft is grounded, the pitot static tube is generally covered.
23. Density is ratio of __________
24. What is the flow of velocity at the top of the cylinder?
25. ___________ is the scalar function of the space and time.