Which of the following is the correct solution of the transformed fundamental equation of aerodynamics for a symmetrical airfoil?

Question

TuteeHUB · Accepted Answer

( )=2 V ( frac {1-cos u2061 theta }{sin theta } )

TuteeHUB · Answer

( )=2 V   (  frac {sin u2061  theta }{1+cos  theta }  )

TuteeHUB · Answer

( )=2 V   (  frac {1+cos  theta }{sin u2061  theta }  )

TuteeHUB · Answer

( )=2 V   (  frac {1-cos u2061  theta }{sin  theta }  )

TuteeHUB · Answer

( )=2 V   (  frac {cos  theta }{sin  theta }  )

1.	Which of the following is the correct solution of the transformed fundamental equation of aerodynamics for a symmetrical airfoil?
A.	( )=2 V<sub> </sub> ( frac {sin u2061 theta }{1+cos theta } )
B.	( )=2 V<sub> </sub> ( frac {1+cos theta }{sin u2061 theta } )
C.	( )=2 V<sub> </sub> ( frac {1-cos u2061 theta }{sin theta } )
D.	( )=2 V<sub> </sub> ( frac {cos theta }{sin theta } )
Answer» C. ( )=2 V<sub> </sub> ( frac {1-cos u2061 theta }{sin theta } )

Discussion