Advanced Search
DSpace@MIT

Blade passage flow structure effects on axial compressor rotating stall inception

Research and Teaching Output of the MIT Community

Show simple item record

dc.contributor.advisor Edward M. Greitzer. en_US
dc.contributor.author Hoying, Donald Andrew en_US
dc.date.accessioned 2005-08-18T17:20:39Z
dc.date.available 2005-08-18T17:20:39Z
dc.date.copyright 1996 en_US
dc.date.issued 1996 en_US
dc.identifier.uri http://hdl.handle.net/1721.1/10623
dc.description Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996. en_US
dc.description Includes bibliographical references (p. 125-130). en_US
dc.description.statementofresponsibility by Donald Andrew Hoying. en_US
dc.format.extent 230 p. en_US
dc.format.extent 13916825 bytes
dc.format.extent 13916580 bytes
dc.format.mimetype application/pdf
dc.format.mimetype application/pdf
dc.language.iso eng en_US
dc.publisher Massachusetts Institute of Technology en_US
dc.rights M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. en_US
dc.rights.uri http://dspace.mit.edu/handle/1721.1/7582
dc.subject Aeronautics and Astronautics en_US
dc.title Blade passage flow structure effects on axial compressor rotating stall inception en_US
dc.type Thesis en_US
dc.description.degree Ph.D. en_US
dc.contributor.department Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics en_US
dc.identifier.oclc 36266242 en_US


Files in this item

Name Size Format Description
36266242.pdf 13.27Mb PDF Preview, non-printable (open to all)
36266242-MIT.pdf 13.27Mb PDF Full printable version (MIT only)

This item appears in the following Collection(s)

Show simple item record

MIT-Mirage