Question: Problem 6 : A Supersonic diffuser for a jet engine is flying at 3 6 0 0 k m h r with atmospheric static pressure

Problem 6: A Supersonic diffuser for a jet engine is flying at 3600kmhr with atmospheric static
pressure and temperature of 20 kPa and -50C, respectively. What is the total pressure loss and the exit
temperature if the diffuser efficiency is 90%? Use Cp=1kJkgK and =1.35.
Problem 6: A Supersonic diffuser for a jet engine is flying at 3600kmhr with atmospheric static
pressure and temperature of 20 kPa and -50C, respectively. What is the total pressure loss and the exit
temperature if the diffuser efficiency is 90%? Use Cp=1kJkgK and =1.35.
Problem 6 : A Supersonic diffuser for a jet

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