Show simple item record

Blade passage flow structure effects on axial compressor rotating stall inception

dc.contributor.advisorEdward M. Greitzer.en_US
dc.contributor.authorHoying, Donald Andrewen_US
dc.date.accessioned2005-08-18T17:20:39Z
dc.date.available2005-08-18T17:20:39Z
dc.date.copyright1996en_US
dc.date.issued1996en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/10623
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.en_US
dc.descriptionIncludes bibliographical references (p. 125-130).en_US
dc.description.statementofresponsibilityby Donald Andrew Hoying.en_US
dc.format.extent230 p.en_US
dc.format.extent13916825 bytes
dc.format.extent13916580 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.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.urihttp://dspace.mit.edu/handle/1721.1/7582
dc.subjectAeronautics and Astronauticsen_US
dc.titleBlade passage flow structure effects on axial compressor rotating stall inceptionen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc36266242en_US


Files in this item

Thumbnail
Name:
36266242-MIT.pdf
Size:
13.27Mb
Format:
PDF
Description:
Full printable version
View/Open

This item appears in the following Collection(s)

Show simple item record