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dc.contributor.advisorJames D. Paduano.en_US
dc.contributor.authorVan Schalkwyk, Christiaan Mauritzen_US
dc.date.accessioned2005-08-18T14:33:44Z
dc.date.available2005-08-18T14:33:44Z
dc.date.copyright1996en_US
dc.date.issued1996en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/10827
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.en_US
dc.descriptionIncludes bibliographical references (p. 179-182).en_US
dc.description.statementofresponsibilityby Christiaan Mauritz Van Schalkwyk.en_US
dc.format.extent182 p.en_US
dc.format.extent8634375 bytes
dc.format.extent8634129 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.titleActive control rotating stall with inlet distortionen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Dept. of Aeronautics and Astronauticsen_US
dc.identifier.oclc35264031en_US


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