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dc.contributor.advisorNorman D. Ham...et al.en_US
dc.contributor.authorShaw, Johnen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-08-04T17:21:17Z
dc.date.available2005-08-04T17:21:17Z
dc.date.copyright1980en_US
dc.date.issued1980en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/15817
dc.descriptionThesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1980.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.en_US
dc.descriptionVita.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby John Shaw.en_US
dc.format.extent2 v. (505 leaves)en_US
dc.format.extent22933622 bytes
dc.format.extent22933382 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.subject.lcshPitching (Aerodynamics)en_US
dc.subject.lcshRotors (Helicopters)en_US
dc.subject.lcshBladesen_US
dc.subject.lcshVibration (Aeronautics) Dampingen_US
dc.titleHigher harmonic blade pitch control : a system for helicopter vibration reductionen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc08043817en_US


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