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The effect of pilot restraint and aerodynamic forces on the flutter of reversible control systems /

Thesis (Ph. D.)--Ohio State University, 1970. / Includes bibliographical references (leaves 72-73). Available online via OhioLINK's ETD Center.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/53785527
Date January 1970
CreatorsMurphy, John Allen,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
SourceConnect to resource

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