A shock wave in air exists in a de Laval nozzle where the cross-sectional area is...

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Mechanical Engineering

A shock wave in air exists in a de Laval nozzle wherethe cross-sectional area is 130cm2.The inletMach number, area and static pressure are 0.35, 210cm2 and 350 kPa. Theexit area of the nozzle is 135cm2.Find:

  • The back pressure for this shock wave tooccur

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SolutionInlet mach number Inlet area Inlet pressure From    See Answer
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