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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Bibliographic Details
Main Author: Srinivasa Murthy, P
Other Authors: Holla, V S
Format: Others
Language:en
Published: Indian Institute of Science 2006
Subjects:
Online Access:http://hdl.handle.net/2005/229