Practice Conservation across a normal shock - 5.1 | 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: Think about the transition between speed regimes.

Question 2

Easy

What is one characteristic of a normal shock?

πŸ’‘ Hint: Consider the pressure behavior when encountering a shock.

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 effect of a normal shock on fluid pressure?

  • Decreases
  • Increases
  • Remains the same

πŸ’‘ Hint: Review how properties change during a shock.

Question 2

True or False: A normal shock is isentropic.

  • True
  • False

πŸ’‘ Hint: Consider the characteristics of isentropic processes.

Solve 1 more question and get performance evaluation

Challenge Problems

Push your limits with challenges.

Question 1

A supersonic airplane is cruising at Mach 2.5. Calculate the change in pressure and temperature as it encounters a normal shock, assuming the initial pressure is 101325 Pa.

πŸ’‘ Hint: You will need to apply the continuity and energy equations appropriately.

Question 2

Discuss the implications of normal shocks on the design of supersonic engines. How do engineers mitigate negative effects?

πŸ’‘ Hint: Consider how aerodynamic shapes contribute to performance.

Challenge and get performance evaluation