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dc.contributor.authorTilton, Edward Lee.en_US
dc.date.accessioned2024-09-16T16:44:30Z
dc.date.available2024-09-16T16:44:30Z
dc.date.copyright1963en_US
dc.date.issued1963en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/156852
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1963en_US
dc.descriptionIncludes bibliographical references (leaf 28).en_US
dc.description.statementofresponsibilityby Edward Lee Tilton, III.en_US
dc.format.extentvii, 42 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.subjectAeronautics and Astronauticsen_US
dc.titleDynamic stability testing with a wind tunnel magnetic model suspension systemen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc34132483en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2024-09-16T16:44:30Zen_US
mit.thesis.degreeMasteren_US


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