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dc.contributor.advisorEdward M. Greizer.en_US
dc.contributor.authorGysling, Daniel Lawrenceen_US
dc.date.accessioned2005-08-15T23:46:28Z
dc.date.available2005-08-15T23:46:28Z
dc.date.copyright1993en_US
dc.date.issued1993en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/12455
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.en_US
dc.descriptionIncludes bibliographical references (p. 250-252).en_US
dc.description.statementofresponsibilityby Daniel L. Gysling.en_US
dc.format.extent347 p.en_US
dc.format.extent17797158 bytes
dc.format.extent17796912 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.titleDynamic control of rotating stall in axial flow compressors using aeromechanical feedbacken_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc29881570en_US


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