Low Reynolds Number Airfoil Aerodynamics
In this thesis we describe the development of Reynolds- averaged Navier Stokes code for the flow past two- dimensional configuration. Particularly, emphasis has been laid on the study of low Reynolds number airfoil aerodynamics. The thesis consists of five chapters covering the back ground history,...
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Format: | Others |
Language: | en |
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Indian Institute of Science
2006
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Online Access: | http://hdl.handle.net/2005/229 |