gas turbine
I.C engine
compressor
air motor
ratio of shaft output of the air motor to the shaft input to the compressor
ratio of shaft input to the compressor to the shaft output of air motor
product of shaft output of air motor and shaft input to the compressor
none of the above
Correct
Incorrect
isothermal
polytropic
isentropic
any one of these
low frontal area
higher thrust
high pressure rise
none of these