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dc.contributor.advisorR. H. Miller.
dc.contributor.authorAmer, Kenneth B.en_US
dc.date.accessioned2024-08-16T22:12:52Z
dc.date.available2024-08-16T22:12:52Z
dc.date.copyright1947en_US
dc.date.issued1947en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/156233
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1947en_US
dc.descriptionBibliography: leaf 27.en_US
dc.description.statementofresponsibilityby Kenneth B. Amer.en_US
dc.format.extentii, 27, [7] leavesen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautical Engineeringen_US
dc.titleThe effect of translation-rotation coupling on helicopter ground resonanceen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc27477295en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Aeronautical Engineeringen_US
dspace.imported2024-08-16T22:12:52Zen_US
mit.thesis.degreeMasteren_US


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