Derive an expression for lift co-efficient of a van de, Mechanical Engineering

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Derive an expression for lift co-efficient of a van de

Derive an expression for lift co-efficient of a Van de Vooren Airfoil having chord length =2l,thickness parameter E and trailing angle tau. Discuss the effects of E and tau on the lift of Van De Vooren Airfoil.

Radius a = 2l(1+E)^k-1/(2^k)

z =(ztilt-a)6k/

(ztilt-aE)^k-1)+ l.

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Mechanical Engineering: Derive an expression for lift co-efficient of a van de

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