In between isothermal and adiabatic
Net work output and work done by turbine
Is independent of clearance volume
Mechanical efficiency
Reduced volume flow rate
Convert kinetic energy into pressure energy
Stagnation pressure at the outlet
All of the above
70 to 90%
As small as possible
Turbine
Mean effective pressure
Discharge pressure
Small quantity of air at high pressure
64 bar
Highly heated atmospheric air
The ratio of the air actually delivered to the amount of piston displacement
High nickel alloy
Is not self operating at zero flight speed