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dc.contributor.advisorRene H. Miller.en_US
dc.contributor.authorShaw, John, Jren_US
dc.date.accessioned2014-04-25T15:46:45Z
dc.date.available2014-04-25T15:46:45Z
dc.date.issued1967en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/86252
dc.descriptionMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. M.S.en_US
dc.descriptionMicrofiche copy available in Barker.en_US
dc.descriptionBibliography: leaves 95-96.en_US
dc.format.extentix, 96 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.titleA feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control.en_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc24013424en_US


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