MCQOPTIONS
Bookmark
Saved Bookmarks
→
Aerodynamics
→
Laminar Flow in Aerodynamics
→
Induced drag is generated by a component of lift ..
1.
Induced drag is generated by a component of lift for a finite wing.
A.
True
B.
False
Answer» B. False
Show Answer
Discussion
No Comment Found
Post Comment
Related MCQs
The total drag coefficient for a wing is given by______
The correct formula for profile drag coefficient over the finite wing is_______
Identify the source which does not cause drag on a finite wing.
The trailing vortex increases the requirement of power by the aircraft engine.
For an inviscid, incompressible flow over finite wings, D’Alembert’s paradox occurs.
Select the incorrect statement for a flow over wings.
Which is the correct statement with regards to the flow over a finite wing?
Induced drag is generated by a component of lift for a finite wing.
For a finite wing, the local airfoil section sees the angle of attack which is called as ____
Reply to Comment
×
Name
*
Email
*
Comment
*
Submit Reply