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I. Analysis of a multi-stage axial compressor with high reaction blading. : II. A design study of a multi-stage axial compressor with blading of high aspect ratio /

Thesis (Aeronautical Engineer). / Includes bibliographical references.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/437063763
Date January 1963
CreatorsMauldin, James H. Rannie, W. Duncan,
PublisherPasadena, Calif. : California Institute of Technology,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
TypeElectronic dissertations.
Source<a href="http://resolver.caltech.edu/CaltechETD:etd-12072005-142501" TARGET="_blank">I. Analysis of a multi-stage axial compressor with high reaction blading. II. A design study of a multi-stage axial compressor with blading of high aspect ratio [electronic thesis]</a>

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