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A study of the effect of boundary layer control on an axial flow compressor stage /

Thesis (Aeronautical Engineer). / Includes bibliographical references.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/437063830
Date January 1954
CreatorsMertz, Charles. Mager, Artur,
PublisherPasadena, Calif. : California Institute of Technology,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
TypeElectronic dissertations.
Source<a href="http://resolver.caltech.edu/CaltechETD:etd-01152004-115145" TARGET="_blank">A study of the effect of boundary layer control on an axial flow compressor stage [electronic thesis]</a>

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