An airplane flying at Mach 0.8 and 10 km altitude (speed of sound a = 230 m/s) has following uninstalled engine measurem

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An airplane flying at Mach 0.8 and 10 km altitude (speed of sound a = 230 m/s) has following uninstalled engine measurem

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An Airplane Flying At Mach 0 8 And 10 Km Altitude Speed Of Sound A 230 M S Has Following Uninstalled Engine Measurem 1
An Airplane Flying At Mach 0 8 And 10 Km Altitude Speed Of Sound A 230 M S Has Following Uninstalled Engine Measurem 1 (19.47 KiB) Viewed 40 times
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.
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