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Contributions to the analysis of high-lift airfoil aerodynamics.

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Author
Lee, Hee Woo
Date
1986-03
Advisor
Platzer, M.F.
Second Reader
Shreeve, Raymond P.
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Abstract
This thesis treats the problem of incompressible two-dimensional steady flow past airfoils or airfoil combinations at large angles of attack. A panel method was developed to compute the inviscid flow over two cylinders, airfoil-flap combinations and airfoils in ground effect. In addition, Cebeci's viscous/inviscid interaction method was applied to several airfoils and compared with available experimental data. The agreement is generally quite encouraging.
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Copyright is reserved by the copyright owner
URI
http://hdl.handle.net/10945/21742
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  • 1. Thesis and Dissertation Collection, all items

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    Integrated Propulsion/Lift/Control System for Aircraft and Ship Applications 

    Platzer, Maximilian F. (The United States of America as represented by the Secretary of the Navy, Washington, DC (US), 1999-11-02);
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    Analysis of incompressible cascade flows using state-of-the-art computer programs. 

    Genskow, Paul E. (1985-03);
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