The lift per unit span for a thin, cambered airfoil with =10 ( frac { – McqOptions

MCQOPTIONS

1.	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____
A.	0
B.	102.55 ( frac {N}{m} )
C.	102.55N
D.	55 ( frac {N}{m} )
Answer» B. 102.55 ( frac {N}{m} )

Discussion

No Comment Found

Related MCQs

The lift per unit span for a thin, cambered airfoil with =10 ( frac {m^2}{s} ), <sub> </sub>=1.0255 ( frac {kg}{m^3} ), V<sub> </sub>=10 ( frac {m}{s} ) is____
The lift per unit span for a thin, cambered airfoil with =5 , A<sub>0</sub>=0.65, A<sub>1</sub>=1 is____
For =5 , A<sub>0</sub>=1 and A<sub>1</sub>=-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<sub> </sub>(A<sub>0</sub> ( frac {1+cos theta }{sin theta } ) + (_{n=1}^ )sin n A<sub>n</sub>) 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<sub> </sub>( - ( 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 A<sub>0</sub>.
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______