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converegent divergent nozzle

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August 16, 2004, 19:07	converegent divergent nozzle	#1
ahmed Guest Posts: n/a	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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