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dc.contributor.advisorEarll M. Murman.en_US
dc.contributor.authorRoberts, Thomas Wesleyen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-08-08T18:15:00Z
dc.date.available2005-08-08T18:15:00Z
dc.date.copyright1987en_US
dc.date.issued1987en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/14907
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1987.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.en_US
dc.descriptionBibliography: leaves 227-233.en_US
dc.description.statementofresponsibilityby Thomas Wesley Roberts.en_US
dc.format.extent2 v. (375 leaves)en_US
dc.format.extent16946780 bytes
dc.format.extent16946536 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 Astronautics.en_US
dc.titleEuler equation computations for the flow over a hovering helicopter rotoren_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc16272868en_US


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