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
›
Aircraft Design
›
The taper ratio of a wing is defined as:
The taper ratio of a wing is defined as:
A. Root chord / tip chord
B. Tip chord / root chord
C. Wingspan / mean chord
D. Area / span
Explanation:
Taper ratio = tip chord / root chord.
Tags:
Aircraft Design
,
Aerospace Engineering
« Previous
Next »
More from Aircraft Design:
Which of the following is the primary objective in aircraft design?
The ratio of wingspan squared to wing area is called:
Which parameter determines how much load an aircraft wing can carry per unit area?
The CG (center of gravity) of an aircraft should be located:
Which of the following reduces induced drag in aircraft design?
In aircraft design, the term "fineness ratio" refers to: