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NACA four-digit airfoil section generation using cubic parametric curve segments and the golden section /

Thesis (M.S.)--Rochester Institute of Technology, 1992. / Typescript. Includes bibliographical references.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/27422477
Date January 1992
CreatorsScarbrough, William T.
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
SourceOnline version of thesis

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