The zero-lift angle of attack for a thin, cambered airfoil increases i – McqOptions

MCQOPTIONS

1.	The zero-lift angle of attack for a thin, cambered airfoil increases in magnitude with the increasing camber of the airfoil.
A.	True
B.	False
Answer» B. False

Discussion

No Comment Found

Related MCQs

The aerodynamic center for all the airfoils lies exactly at the quarter-chord always for all the given angle of attacks.
When the lift becomes zero, the center of pressure of the cambered airfoil is at which point on the airfoil (consider given lengths are from the leading edge)?
For a cambered airfoil, the center of pressure does not vary with_____
The quarter-chord is the aerodynamic center for a cambered airfoil.
The quarter-chord is the center of pressure for a cambered airfoil.
The quarter-chord moment coefficient for a cambered airfoil depends on______
Given an angle of attack 5 , A<sub>1</sub>=1.5, A<sub>2</sub>=2 and the chord length is 5m, the moment coefficient about the quarter-chord is_____
The relation between lift coefficient and moment coefficient about the leading edge is_______
The moment coefficient for a thin cambered airfoil about the leading edge is given by______
The zero-lift angle of attack for a thin, cambered airfoil increases in magnitude with the increasing camber of the airfoil.