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dc.contributor.advisorEugene E. Covert.en_US
dc.contributor.authorRamer, Becky E. (Becky Ellen)en_US
dc.date.accessioned2009-12-10T18:53:41Z
dc.date.available2009-12-10T18:53:41Z
dc.date.copyright1997en_US
dc.date.issued1997en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/49964
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.en_US
dc.descriptionIncludes bibliographical references (leaves 75-76).en_US
dc.description.statementofresponsibilityby Becky E. Ramer.en_US
dc.format.extent76 leavesen_US
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/1721.1/7582en_US
dc.subjectAeronautics and Astronauticsen_US
dc.titleAerodynamic response of turbomachinery blade rows to convecting density distortionsen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc36822411en_US


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