The incorrect difference between airfoil and wings is_______ – McqOptions

MCQOPTIONS

1.	The incorrect difference between airfoil and wings is_______
A.	Presence of induced drag in wings
B.	Different effective angles of attack seen by
C.	Difference in the lift-curve slope
D.	Lift slope of the wing is higher than of airfoil
Answer» E.

Discussion

No Comment Found

Related MCQs

For very high aspect ratio wings, the lift curve slope resembles that of the airfoil.
The values of lift slope for elliptic wing (a<sub>e</sub>) and general planform wing (a) is less than that for airfoil (a<sub>0</sub>).<br>Mark the false statement.
For a finite wing and an infinite wing (airfoil), zero lift angle of attack is zero.
The incorrect difference between airfoil and wings is_______
Tapered wings are used more rather than elliptical wing planforms practically. The reason being______
The elliptical lift distribution has a major interest in making wings because_____
Select the incorrect equation for the induced drag coefficient for a finite wing.
The incorrect choice for the general lift distribution for a finite wing is ________
For an elliptical lift distribution, the planform area is also elliptical for a wing.
The incorrect statement for a finite wing with elliptical lift distribution out of the following is_____