Exam
Vibe
Home
Engineering
Aerospace Engineering
Biomedical Engineering
Chemical Engineering
Civil Engineering
Computer Science
Electrical Engineering
Electronics and Communication Engineering
Mechanical Engineering
Govt Exam
Banking Exams
Other Government
Police
Railway Exams
SSC
State PSC Exams
Teaching / Education Exams
UPSC Exams
Blog
Contact
🔍
Home
›
Aerospace Engineering
›
Propulsion MCQ
›
The bypass ratio in a turbofan engine is defined as:
The bypass ratio in a turbofan engine is defined as:
A. Air mass bypassing the engine to air mass passing through core
B. Fuel-air ratio
C. Thrust-weight ratio
D. Compressor pressure ratio
Explanation:
Bypass ratio = mass flow of bypass air / mass flow through core.
Tags:
Propulsion MCQ
,
Aerospace Engineering
« Previous
Next »
More from Propulsion MCQ:
The main purpose of an aircraft propulsion system is to:
Which of the following is a type of aircraft engine?
In a turbojet engine, the main components include:
Which engine type is most fuel-efficient for subsonic transport aircraft?
Which component of a jet engine drives the compressor?
Afterburners are used to: