- #1
sarahqwert
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Homework Statement
a converging diverging nozzle is operating at sea level, it will be mounted on a glider that flies 26.8m/s. The entrance area is 1 m^2.
Homework Equations
what is the stagnation pressure and mach number of flow entering the nozzle? what should be throat and exit area if exit mach number is 2?
3.
at entrance M=V/a = 26.8/346 = .077
so P/P0 =.669
we are not given P so how do we find P0?