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PLEASE answer all questions clearlyProblem 6.109 SI As shown in the figure below, air enters the diffuser of a jet engine at 18 kPa, Ti 250 K with a velocity of V1 = 201 m/s, all data corresponding to high-altitude flight. The air flows adiabatically through the diffuser, decelerating to a velocity of 50 m/s at the diffuser exit. DiffuserCompressor Combustors Giurbine -Nozzle P1-18 kPa Ti,V V2-50 m/s Air Product in gases out Assume steady-state operation, the ideal gas model for air, and negligible potential energy effects. (a) Determine the temperature of the air at the exit of the diffuser, in K. (b) If the air would undergo an isentropic process as it flows through the diffuser, determine the pressure of the air at the diffuser exit, in kPa. (c) If friction were present, would the pressure of the air at the diffuser exit be greater than, less than, or equal to the value found in part (b)?

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ven thah = 250k Fnean balance fur thiz Syem 2. 2 2- 50 -20 → h: 250.05 2 h2201- 31 + h,

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