Practice Key relations - 3.1 | 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 fluid density in compressible flows?

πŸ’‘ Hint: Think about what happens to gases at different speeds.

Question 2

Easy

Define stagnation temperature.

πŸ’‘ Hint: Recall the conditions of no heat transfer.

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 defines compressible flow?

  • A): Flows that can be compressed easily
  • B): Flows with negligible density change
  • C): Flows with significant density changes due to pressure/temperature variations

πŸ’‘ Hint: Think about speed and density.

Question 2

True or False: Stagnation properties are values at rest under isentropic conditions.

  • True
  • False

πŸ’‘ Hint: Consider definitions of temperature and properties.

Solve 1 more question and get performance evaluation

Challenge Problems

Push your limits with challenges.

Question 1

A supersonic aircraft is cruising at a Mach number of 2.5. Calculate the change in pressure and temperature across a normal shock experienced when the aircraft slows down to a Mach number of 0.8.

πŸ’‘ Hint: Setup equations for conservation principles.

Question 2

A nozzle is designed for a fluent flow with an initial pressure of 200 kPa and temperature of 300 K. Determine the area at the throat if the Mach number needs to be maintained at 2.0.

πŸ’‘ Hint: Remember to rearrange equations to solve for area.

Challenge and get performance evaluation