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dc.contributor.authorChow, H. Ken_US
dc.contributor.otherMassachusetts Institute of Technology. Aeronautical Engineering Department.
dc.date.accessioned2009-03-16T19:56:49Z
dc.date.available2009-03-16T19:56:49Z
dc.date.issued1915en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/44893
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1915.en_US
dc.description.statementofresponsibilityby H. K. Chow.en_US
dc.format.extent1 v. in various pagingsen_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.subjectAeronautical Engineering Dept.en_US
dc.titleExperimental determination of damping coefficients in the stability of aeroplanesen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc38141318en_US


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