An airplane flying at Mach 0.8 and 10 km altitude (speed of sound a = 230 m/s) has following uninstalled engine measurem
Posted: Mon May 16, 2022 12:14 am
An airplane flying at Mach 0.8 and 10 km altitude (speed of sound a = 230 m/s) has following uninstalled engine measurement: Air mass flow rate mo = 50 kg/s Fuel mass flow rate m= 2.55 kg/s Exhaust velocity Ve = 1250 m/s Calculate the uninstalled thrust F and the net power out of engine W ont.