Fluid Mechancis
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Fluid Mechancis March 2015 If a shockwave is in the diverging section i.e between exit & throat then First use A y /A * y , calculate A * y & then use A exit /A * y to calculate Ma exit . But if the Shock wave appears at the end face then the Ma exit = Ma x &soP exit = P x , calculatetheP y = P back . 1
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Transcript of Fluid Mechancis
Fluid Mechancis
March 2015
If a shockwave is in the diverging section i.e between exit & throat then First useAy/A
∗y, calculate A∗
y & then use Aexit/A∗yto calculate Maexit.
But if the Shock wave appears at the end face then the Maexit = Max&soPexit =Px, calculatethePy = Pback.
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