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
›
Helicopter Engineering MCQ
›
Torque effect in helicopters is countered by:
Torque effect in helicopters is countered by:
A. Main rotor speed reduction
B. Tail rotor or NOTAR system
C. Cyclic control
D. Landing gear design
Explanation:
Tail rotor or NOTAR systems balance main rotor torque.
Tags:
Helicopter Engineering MCQ
,
Aerospace Engineering
« Previous
Next »
More from Helicopter Engineering MCQ:
Which rotor type is commonly used in helicopters for lift?
The tail rotor in a helicopter primarily prevents:
Which control changes the pitch of all rotor blades simultaneously?
Cyclic control in a helicopter is used to:
The term “autorotation” refers to:
A helicopter’s center of gravity affects:
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