Can flow become supersonic in a converging nozzle?
no
@@sirigiabhiram7924 why?
@@rahuljaiswal7253 because after reaching mach 1 the pressure wave from downstream can't penetrate into upstream flow so upstream condition no longer varied by download stream condition so we can't achieve supersonic
@@sirigiabhiram7924 can u send mathematical proof
@@rahuljaiswal7253 if u differentiate mass flow rate equation you will get M=1
Can flow become supersonic in a converging nozzle?
no
@@sirigiabhiram7924 why?
@@rahuljaiswal7253 because after reaching mach 1 the pressure wave from downstream can't penetrate into upstream flow so upstream condition no longer varied by download stream condition so we can't achieve supersonic
@@sirigiabhiram7924 can u send mathematical proof
@@rahuljaiswal7253 if u differentiate mass flow rate equation you will get M=1