Practice Normal Shocks - 5 | Compressible Flow | Applied Thermodynamics
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Practice Questions

Test your understanding with targeted questions related to the topic.

Question 1

Easy

What happens to the Mach number across a normal shock?

πŸ’‘ Hint: Recall the transition from supersonic to subsonic flow.

Question 2

Easy

Name one property that increases across a normal shock.

πŸ’‘ Hint: Think about what happens when a shock compresses the flow.

Practice 4 more questions and get performance evaluation

Interactive Quizzes

Engage in quick quizzes to reinforce what you've learned and check your comprehension.

Question 1

What is the primary effect of a normal shock on flow?

  • Decrease in pressure
  • Increase in Mach number
  • Decrease in Mach number

πŸ’‘ Hint: Think about the transition happening in supersonic conditions.

Question 2

True or False: Normal shocks are isentropic.

  • True
  • False

πŸ’‘ Hint: What does entropy signify in fluid dynamics?

Solve 2 more questions and get performance evaluation

Challenge Problems

Push your limits with challenges.

Question 1

A supersonic jet with a Mach number of 1.5 experiences a normal shock. Determine the downstream Mach number and corresponding change in pressure if the initial pressure is 100 kPa.

πŸ’‘ Hint: Use the standard relationships for pressure and density changes across shocks.

Question 2

Analyze how a normal shock would influence the design of a supersonic passenger aircraft. What factors must be addressed?

πŸ’‘ Hint: Consider aerodynamic shape, material stresses, and engine performance.

Challenge and get performance evaluation