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

by: Mauldin, James H.

Publication date: 1963

Topics: Aeronautics

Publisher: California Institute of Technology

Collection: navalpostgraduateschoollibrary; fedlink; americana

Contributor: Naval Postgraduate School, Dudley Knox Library

Language: en_US

Thesis (Ae. E.)--California Institute of Technology, 1963

Includes bibliographies

Addeddate: 2012-01-21 03:54:00

Associated-names: California Institute of Technology

Call number: ocn437063763

Camera: Canon EOS 5D Mark II

Degree.discipline: Aeronautical Engineering

Degree.grantor: California Institute of Technology

Degree.level: professional degree

Degree.name: Degree of Aeronautical Engineer

Description.service: U.S. Navy (U.S.N.) author.

External-identifier: urn:handle:10945/12809
urn:oclc:record:1050267381

Foldoutcount: 0

Identifier: partianalysisofm00maul

Full catalog record: MARCXML

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

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