provides greater flexibility

provides lesser flexibility

in never used

is used when gas is to be burnt

compressor work and turbine work

output and input

actual total head tempeature drop to the isentrpic total head drop from total head inlet to static head outlet

actual compressor work and theoretical comprssor work

adiabatic temperature drop in the stage

total temperature drop

total temperature drop in the stage

total adiabaitc temperature drop

isothermal

isentropic

adiabatic

isochoric

gas turbine uses low air-fuel ratio to economise on fuel

gas turhine uses high air-fuel ratio to reduce outgoing temperature

gas turbine uses low air-fuel ratio to develop the high thrust required

all of the above