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In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine by burning, more fuel is used to increase the
The maximum propulsion efficiency of a turbojet is attained at around following speed
A turboprop is preferred to turbojet because
The maximum propulsive efficiency of a turbojet engine is at a speed of
The turbine of the turboprop engine is __________ that of the turbojet engine.
A simple turbojet engine is basically
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is
Ram compression in turbojet involves
In turbo fan engine, the jet velocity as compared to turbojet engine is
The fuels in order of decreasing knock tendency for spark ignition engines are