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Under What Circumstances Would There Be An Increase In Pressure In A Diver¬gent Nozzle ?

Answer»

For SUBSONIC flow at INLET SECTION of a diffuser a lower velocity and HIGHER pressure will exist at the exit section. For supersonic isentropic flow at the inlet section a higher velocity and lower pressure will exist at the exit but if a SHOCK wave occurs in the diffuser then a higher pressure will exist at the exit.

For subsonic flow at inlet section of a diffuser a lower velocity and higher pressure will exist at the exit section. For supersonic isentropic flow at the inlet section a higher velocity and lower pressure will exist at the exit but if a shock wave occurs in the diffuser then a higher pressure will exist at the exit.



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