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

Question

TuteeHUB · Accepted Answer

γ(θ)=2αV∞$\frac {1-cos⁡\theta }{sin\theta }$

TuteeHUB · Answer

γ(θ)=2αV∞$\frac {sin⁡\theta }{1+cos\theta }$

TuteeHUB · Answer

γ(θ)=2αV∞$\frac {1+cos\theta }{sin⁡\theta }$

TuteeHUB · Answer

γ(θ)=2αV∞$\frac {1-cos⁡\theta }{sin\theta }$

TuteeHUB · Answer

γ(θ)=2αV∞$\frac {cos\theta }{sin\theta }$

1.	Which of the following is the correct solution of the transformed fundamental equation of aerodynamics for a symmetrical airfoil?
A.	γ(θ)=2αV∞\(\frac {sin⁡\theta }{1+cos\theta }\)
B.	γ(θ)=2αV∞\(\frac {1+cos\theta }{sin⁡\theta }\)
C.	γ(θ)=2αV∞\(\frac {1-cos⁡\theta }{sin\theta }\)
D.	γ(θ)=2αV∞\(\frac {cos\theta }{sin\theta }\)
Answer» C. γ(θ)=2αV∞\(\frac {1-cos⁡\theta }{sin\theta }\)

Discussion