MCQOPTIONS
Bookmark
Saved Bookmarks
→
Aerodynamics
→
Laminar Flow
→
For an angle of attack of 5 and slope of camber l...
1.
For an angle of attack of 5 and slope of camber line being zero, find the value of A0.
A.
0.087
B.
5
C.
0
D.
-5
Answer» B. 5
Show Answer
Discussion
No Comment Found
Post Comment
Related MCQs
The lift per unit span for a thin, cambered airfoil with =10 ( frac {m^2}{s} ), =1.0255 ( frac {kg}{m^3} ), V =10 ( frac {m}{s} ) is____
The lift per unit span for a thin, cambered airfoil with =5 , A0=0.65, A1=1 is____
For =5 , A0=1 and A1=-2 total circulation for a thin cambered airfoil equals______
The correct formula for the Fourier sine series appearing in the solution of thin airfoil theory is_____
For ( )=2V (A0 ( frac {1+cos theta }{sin theta } ) + (_{n=1}^ )sin n An) select the statement which is invalid.
Select the statement which is not true for the solution of ( frac {1}{2 pi } int_0^c frac { gamma( xi)d xi}{x- xi} )=V ( - ( frac {dz}{dx} )) for a cambered airfoil.
For an angle of attack of 5 and slope of camber line being zero, find the value of A0.
NACA 0023 is______
For NACA4313 what is the maximum camber and the position of maximum camber from the leading edge respectively is______
The extra term appearing in the thin airfoil theory solution for a cambered airfoil is a______
Reply to Comment
×
Name
*
Email
*
Comment
*
Submit Reply