2026-09-19T16:58:00Zhttps://dspace.mit.edu/server/oai/requestoai:dspace.mit.edu:1721.1/106232022-01-13T07:54:10Zcom_1721.1_7582com_1721.1_7581col_1721.1_131022
Edward M. Greitzer.
Hoying, Donald Andrew
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
2005-08-18T17:20:39Z
2005-08-18T17:20:39Z
1996
1996
http://hdl.handle.net/1721.1/10623
36266242
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.
Includes bibliographical references (p. 125-130).
by Donald Andrew Hoying.
Ph.D.
230 p.
13916825 bytes
13916580 bytes
application/pdf
application/pdf
eng
Massachusetts Institute of Technology
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.
http://dspace.mit.edu/handle/1721.1/7582
Aeronautics and Astronautics
Blade passage flow structure effects on axial compressor rotating stall inception
Thesis
application/pdf
false
Publication
unknown
unknown
<Publication xmlns="https://www.openaire.eu/cerif-profile/1.1/" id="f104ab8e-189c-4ad3-87b9-e9f2dc3f016a">
<Type xmlns="https://www.openaire.eu/cerif-profile/vocab/COAR_Publication_Types">http://purl.org/coar/resource_type/c_1843</Type>
<Language>eng</Language>
<Title>Blade passage flow structure effects on axial compressor rotating stall inception</Title>
<PublishedIn>
<Publication>
</Publication>
</PublishedIn>
<PublicationDate>1996</PublicationDate>
<Authors>
<Author>
<DisplayName>Hoying, Donald Andrew</DisplayName>
<Affiliation>
<OrgUnit>
</OrgUnit>
</Affiliation>
</Author>
</Authors>
<Editors>
</Editors>
<Publishers>
<Publisher>
<DisplayName>Massachusetts Institute of Technology</DisplayName>
<OrgUnit />
</Publisher>
</Publishers>
<License>http://dspace.mit.edu/handle/1721.1/7582</License>
<Keyword>Aeronautics and Astronautics</Keyword>
<Access xmlns="http://purl.org/coar/access_right"
>
</Access>
</Publication>