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Derive an expression for the Mach number after a normal shock wave occurring in a nozzle.
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Sep 5, 2017
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FM&Compressible
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chandu
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Derive an expression for the Mach number after a normal shock wave occurring in a nozzle. Show the trend of this Mach number, (in the form of an x-y plot) with respect to the Mach number value before the shock.
iasmains
2009
fm&compressible
shock-wave
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