Air at 100 kPa, 15oC, and 300 m/s enters the adiabatic diffuser of a jet engine steadily.

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Air at 100 kPa, 15oC, and 300 m/s enters the adiabatic diffuser of a jet engine steadily. The inlet area of the diffuser is 0.4 m2, and exit area of the diffuser is 1 m2. Using the Diffuser Simulator (linked from the left margin), calculate:
Exit pressure (p2).
Exit temperature (T2).
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