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
›
Gas Turbine Engines MCQ
›
The bypass ratio of a turbofan engine is define...
The bypass ratio of a turbofan engine is defined as:
A. Fuel-to-air ratio
B. Mass flow of bypass air to core air
C. Exhaust velocity to inlet velocity
D. Thrust-to-weight ratio
Explanation:
Bypass ratio compares the air bypassing the core to the air going through the core.
Tags:
Gas Turbine Engines MCQ
,
Aerospace Engineering
« Previous
Next »
More from Gas Turbine Engines MCQ:
What is the primary function of a gas turbine engine in aircraft?
In a turbofan engine, most of the thrust is produced by:
The Brayton cycle is the thermodynamic cycle of:
The compressor in a gas turbine engine is used to:
Which of the following is a type of gas turbine engine?
What is the main disadvantage of turbojet engines compared to turbofans?
Explore more in Aerospace Engineering:
Aerodynamics MCQs MCQs
Flight Mechanics MCQ MCQs
Aircraft Structures MCQs
Propulsion MCQ MCQs
Avionics MCQ MCQs
Aircraft Design MCQs
Spacecraft Engineering MCQ MCQs
Orbital Mechanics MCQ MCQs
Aerospace Materials MCQ MCQs
Flight Testing MCQ MCQs