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dc.contributor.advisorC. Fayette Taylor.en_US
dc.contributor.authorVan Alstyne, Harold Leroyen_US
dc.contributor.otherMassachusetts Institute of Technology. Aeronautical Engineering Department.
dc.date.accessioned2018-11-15T16:37:29Z
dc.date.available2018-11-15T16:37:29Z
dc.date.issued1927en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/119121
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1927.en_US
dc.description.statementofresponsibilityby Harold Leroy Van Alstyne.en_US
dc.format.extent45 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautical Engineering Dept.en_US
dc.titleAn investigation of the bending moments imposed upon the crank pin end of the master rod of the Wright J-5, radial, air-cooled aviation engineen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc36830140en_US


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