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converegent divergent nozzle

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Old   August 16, 2004, 19:07
Default converegent divergent nozzle
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ahmed
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hello people i am looking for a formulae for a convergeent divergent nozzle,which can relate the exit mach number to the inlet mach number for compressible flow.this formulae relates the area ratio of the throat and the exit of the nozzle. thanks
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