Q.

The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

  • AIncreases
  • BDecreases
  • CFirst increases and then decreases
  • DFirst decreases and then increases
Correct Answer : (A)

Increases

Hints :
Previous

The temperature of air at the beginning of the compression stroke is ________ the atmospheric temperature.

Next

The assumption made in two stage compression with inter-cooler is that

Join The Discussion