Course Assessment — Compressible Flow and Shock Waves
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Question 1 of 10
1. Question
What is a perfect gas?
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Question 2 of 10
2. Question
What is the Mach number?
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Question 3 of 10
3. Question
What is a normal shock?
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Question 4 of 10
4. Question
What is the impact of a normal shock on a supersonic flow?
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Question 5 of 10
5. Question
What are Mark waves?
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Question 6 of 10
6. Question
What does the area-velocity relation explain?
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Question 7 of 10
7. Question
What is the maximum Mach number that can be achieved at the throat of a converging-diverging nozzle?
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Question 8 of 10
8. Question
What happens when the Mach number reaches 1 at the throat of a nozzle?
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Question 9 of 10
9. Question
What is the impact of shock waves on the aerodynamic performance of an airfoil?
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Question 10 of 10
10. Question
What is the purpose of the diaphragm in a shock tube?