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Numerical investigation of the effect of leading edge geometry on dynamic stall of airfoils

Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, September 1990. / Thesis Advisor(s): Ekaterinaris, John A. ; Platzer, Max. "September 1990." Description based on title screen as viewed on December 21, 2009. DTIC Identifier(s): Dynamics, leading edges, airfoils, dynamic stall, oscillating airfoil, pitching airfoil, leading edge geometry, pressure gradient, theses. Author(s) subject terms: Dynamic stall, oscillating airfoil, pitching airfoil, leading edge geometry, pressure gradient. Includes bibliographical references (p. 111-112). Also available in print.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/491292791
Date January 1990
CreatorsGrohsmeyer, Steven P.
PublisherMonterey, California : Naval Postgraduate School,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
Source(5.72 MB)

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