Elevator provides control for ______ – McqOptions

MCQOPTIONS

Saved Bookmarks

→ Aircraft Design
→ Longitudinal Static Stability Control 1 in Aircraft Design
→ Elevator provides control for ______..

1.	Elevator provides control for ______
A.	pitching moment
B.	yawing
C.	roll
D.	yaw-roll
Answer» B. yawing

Discussion

No Comment Found

Related MCQs

What is the use of V type tail?
Determine the corrections or otherwise of the following assertion [A] and reason [R]:Assertion [A]: Most of the tails are using symmetric airfoils.Reason[R]: Tail control has two primary control surface.
The inverted V-tail is used to ______
Which of the following is not part of tail?
Typically, high speed aircrafts have thinner tail as compared to wing thickness.
Glider with span of 2m is flying at 10000ft. If aspect ratio of tail is 10 then, determine reference area of the tail.
Elevator provides control for ______
Which control surface is primarily used for spin recovery?
Why dorsal fins are used?
Horizontal stabilizer is away from wing wake in T-tail configuration.

Related Topics

Longitudinal Static Stability Control 1 in Aircraft Design

Conceptual Sketch Sizing Takeoff Weight Buildup in Aircraft Design

Crew Station in Aircraft Design

Configuration Layout Considerations Aural Signature in Aircraft Design

Subsystems in Aircraft Design

Airfoil Selection 1 in Aircraft Design

Configuration Layout Wing Tail Layout Loft 1 in Aircraft Design

Configuration Layout Conic Fuselage Development in Aircraft Design

Loads Categories in Aircraft Design

Flight Mechanics Level Turning Flight in Aircraft Design

Recent Visits

Reply to Comment

Name *

Email *

Comment *

© Copyright 2025 McqOptions. All rights reserved.

Terms & Conditions
Privacy Policy
Disclaimer

Support: admin@mcqoptions.com