The effects of trailing edge bluntness on airfoil performance as calculated approximately by a viscid-inviscid vortex panel method

Author(s)
D'Angelo, Michael R. (Michael Ronald)
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Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Advisor
Eugene E. Covert.
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Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.
 
Includes bibliographical references (leaves 86-88).
 
Date issued
1989
URI
http://hdl.handle.net/1721.1/39013
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Publisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics.
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