LiftingFlows

LiftingFlows - MEM420 Aerodynamics Dr. A. Yousuff...

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MEM420 Aerodynamics Dr. A. Yousuff MEM/Drexel
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overview yousuff Aerodynamics 2 Non-lifting flow over a cylinder Lifting flow over a cylinder Kutta-Joukowsky Theorem (L = V ) Panel Method
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Uniform flow + doublet yousuff Aerodynamics 3 22 2 1 cos , 1 sin 2 , r R wi t hR V    
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Non-lifting flow over a cylinder yousuff Aerodynamics 4 The Streamline = 0 (circle) separates the flow from doublet and uniform. Uniform flow over a cylinder.
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observations yousuff Aerodynamics 5 0; 2 sin r V   @ , 2 2  
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Uniform flow + doublet + vortex yousuff Aerodynamics 6
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Stagnation points yousuff Aerodynamics 7 2 2 1 c s 0 o r R V    2 2 2 1 sin    2 2 2 2 1 44     
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Stagnation points, contd.
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This note was uploaded on 04/26/2011 for the course MEM 420 taught by Professor Ajamal during the Spring '11 term at Drexel.

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LiftingFlows - MEM420 Aerodynamics Dr. A. Yousuff...

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