Propulsive efficiency is defined as ratio of

Home / Mechanical Engineering / Compressors, Gas Turbines And Jet Engines / Question

Examveda

A. Thrust power and fuel energy

B. Engine output and propulsive power

C. Propulsive power and fuel input

D. Thrust power and propulsive power

Answer: Option D

Solution (By Examveda Team)

Propulsive efficiency is defined as ratio of Thrust power and propulsive power

Related Questions on Compressors, Gas Turbines and Jet Engines

A. Equal to

B. Less than

C. More than

D. None of these

View Answer

A. At the base

B. At the tip

C. In the center

D. Between ~ to i of the blade height

View Answer

A. Higher

B. Lower

C. Equal

D. Can't be compared

View Answer

A. 200°C

B. 500°C

C. 700°C

D. 1000°C

View Answer