Maurice Tutor

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    Argosy University/ Phoniex University/
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    Phoniex University
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Category > Management Posted 13 Oct 2017 My Price 2.00

aircraft flies

An aircraft flies with a Mach number Ma1 =0.8 at an altitude of 7000 m where the pressure is 41.1 kPa and the temperature is 242.7 K. The diffuser at the engine inlet has an exit Mach number of Ma2 =0.3. For a mass flow rate of 65 kg/s, determine the static pressure rise across the diffuser and the exit area.

 

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Maurice Tutor
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Status NEW Posted 13 Oct 2017 06:10 PM My Price 2.00

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