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

Description

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

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1. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=osu1225726005

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Identifer	oai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/53785527
Date	January 1970
Creators	Murphy, John Allen,
Source Sets	OCLC
Language	English
Detected Language	English
Source	Connect to resource