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Physics, 16.11.2019 05:31 AgarioEdit

Air enters the diffuser of a jet engine operating at steady state at 18 kpa, 216 k and a velocity of 265 m/s, all data corresponding to high-altitude flight. the air flows adiabatically through the diffuser and achieves a temperature of 250 k at the diffuser exit. using the ideal gas model for air, determine the velocity of the air at the diffuser exit,

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