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

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

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.

Bibliografische gegevens
Hoofdauteur: D'Angelo, Michael R. (Michael Ronald)
Andere auteurs: Eugene E. Covert.
Formaat: Thesis
Taal:eng
Gepubliceerd in: Massachusetts Institute of Technology 2007
Onderwerpen:
Aeronautics and Astronautics.
Online toegang:http://hdl.handle.net/1721.1/39013

Internet

http://hdl.handle.net/1721.1/39013

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