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A numerical vortex approach to aerodynamic modeling of SUAV/VTOL aircraft /

Thesis (M.S.)--Brigham Young University. Dept. of Mechanical Engineering, 2007. / Includes bibliographical references (p. 73-74).

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/367989471
Date January 2007
CreatorsHunsaker, Douglas F.,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
TypeElectronic dissertations.
SourceCLICK HERE for online access

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