MCQOPTIONS
Bookmark
Saved Bookmarks
→
Aerodynamics
→
Laminar Flow in Aerodynamics
→
The lift curve slope for a flat plate is_____..
1.
The lift curve slope for a flat plate is_____
A.
2π rad
B.
2π rad-1
C.
π rad
D.
0.11 degree
Answer» C. π rad
Show Answer
Discussion
No Comment Found
Post Comment
Related MCQs
Aerodynamic center and center of pressure coincide for all the airfoils.
For a flat plate, aerodynamic center and center of pressure coincide.
Select the incorrect statement for a thin, symmetric airfoil out of the following.
The coefficient of moment about the quarter chord is zero for a symmetric airfoil. This implies____
Which of the following is an incorrect relation for a flat plate?
Given an angle of attack 5° and c = 5m, the moment coefficient about the leading edge is_____
The lift curve slope for a flat plate is_____
The lift coefficient for a thin symmetrical airfoil is given by______
Which of these is a wrong expression for the total circulation around a thin symmetric airfoil?
What is the total circulation around the symmetric airfoil according to the thin airfoil theory?
Reply to Comment
×
Name
*
Email
*
Comment
*
Submit Reply