The exit nozzle in a jet engine receives air at 1200 K,

Chapter 7, Problem 16HP

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QUESTION:

Problem 16HP

The exit nozzle in a jet engine receives air at 1200 K, 150 kPa with negligible kinetic energy. The exit pressure is 80 kPa, and the process is reversible and adiabatic. Use constant specific heat at 300 K to find the exit velocity.

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QUESTION:

Problem 16HP

The exit nozzle in a jet engine receives air at 1200 K, 150 kPa with negligible kinetic energy. The exit pressure is 80 kPa, and the process is reversible and adiabatic. Use constant specific heat at 300 K to find the exit velocity.

ANSWER:

Solution 16 HP

Step 1 of 4

To find the velocity of nozzle at the exit state.

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