ExamVeda
Login
Home

In gas turbines high thermal efficiency is obtained in

This question belongs to Mechanical Engineering Compressors, Gas Turbines And Jet Engines
Compressors, Gas Turbines and Jet Engines
?

In gas turbines, high thermal efficiency is obtained in

Answer & Solution
Correct Answer: Option A
In gas turbines, high thermal efficiency is obtained in closed cycle
Examveda
Question posted by Examveda
Community

Join the Discussion

No comments yet Be the first to discuss this question.
Keep Learning

Related Questions on Compressors, Gas Turbines and Jet Engines

The compression ratio for the compressor is always _________ unity.
A. Equal to B. Less than C. More than D. None of these
The hottest point in a gas turbine is
A. At the base B. At the tip C. In the center D. Between ~ to i of the blade height
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is
A. Higher B. Lower C. Equal D. Can't be compared
The maximum temperature in a gas turbine is
A. 200°C B. 500°C C. 700°C D. 1000°C
More Related Questions on Compressors, Gas Turbines and Jet Engines