Consider a convergent-divergent duct with an exit-to-throat area ratio of 1.6. Calculate the exit-to-reservoir pressure ratio required
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Consider a convergent-divergent duct with an exit-to-throat area ratio of 1.6. Calculate the exit-to-reservoir pressure ratio required to achieve sonic flow at the throat, but subsonic flow everywhere else.
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Since M1 at the throat AtA Thus fracAeAtfracAeA16 From Table A1 the ...View the full answer
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