Poor wing fuselage will reduce lift loss. – McqOptions

MCQOPTIONS

Saved Bookmarks

→ Aircraft Design
→ Longitudinal Static Stability Control 1 in Aircraft Design
→ Poor wing fuselage will reduce lift loss...

1.	Poor wing fuselage will reduce lift loss.
A.	True
B.	False
Answer» C.

Discussion

No Comment Found

Related MCQs

Determine the corrections or otherwise of the following assertion [A] and reason [R]:<br>Assertion [A]: Maintaining smooth longitudinal contour in fuselage will give better aerodynamic design.
What is the disadvantage of short and fat fuselage?
Short and fat fuselage will have ___________
To reduce fuselage wetted area we can ___________
___________ can be considered as one of the most powerful aerodynamic consideration.
If an aircraft is not designed properly then __________
Poor wing fuselage will reduce lift loss.

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