constant expansion with heat addition, then constant volume

with internal heat transfer from the working fluid to a regenerator, then

constant compression with heat rejection, then constant volume with internal

heat transfer from the regenerator back to the working fluid

Isentropic

compression, then Constant-pressure heat addition, then Isentropic expansion,

then Constant-volume heat rejection

Isentropic compression, then

Constant-volume heat addition, then Isentropic expansion, then Constant-volume

heat rejection

Isentropic compression, then

Constant-pressure heat addition, then Isentropic expansion, then

Constant-pressure heat rejection

Isentropic compression, then

Constant-pressure heat rejection, then throttling, then Constant-pressure heat

absorption

The

air enters the combustion chamber at the turbine exit temperature.

The

temperature of the air entering the combustion chamber is higher than the

turbine exit temperature.

The exhaust temperature is

reduced to the minimum theoretical temperature.

The

exhaust temperature is lower than the compressor exit temperature.

Increases the fuel added to the

cycle.

Increases the possibility of NOx

formation.

Increases the temperature of the

exhaust gases.

Requires

improved cooling techniques for the turbine blades.

The

turbine work is significantly higher than the compressor work.

The irreversibility in the cycle increases

the produced thrust.

The isothermal reversible

work.

The

actual work.

The

adiabatic reversible work.