Engineering
Engineering, 11.07.2019 03:20, ringo12384

Determine the specific thrust for a turbojet engine flying at m-0.85 at an altitude of 1 m. assume a compressor pressure ratio of 30, turbine inlet temperature of 1400 k, and compressor and turbine efficiencies of 0.85 and 0.90, respectively

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Determine the specific thrust for a turbojet engine flying at m-0.85 at an altitude of 1 m. assume a...

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