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Low-frequency describing function models for the Atlas missile thrust chamber electrohydraulic position servo with application to determining rigid-body and propellant-sloshing limit cycles

Thesis (M.S.)--University of Wisconsin--Madison, 1968. / eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/609240818
Date January 1968
CreatorsHermann, Fred William,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish

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