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)![Thumbnail](/bitstream/handle/1721.1/39013/20404644-MIT.pdf.jpg?sequence=5&isAllowed=y)
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Other Contributors
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Advisor
Eugene E. Covert.
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Metadata
Show full item recordDescription
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989. Includes bibliographical references (leaves 86-88).
Date issued
1989Department
Massachusetts Institute of Technology. Department of Aeronautics and AstronauticsPublisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics.