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dc.contributor.authorDoolittle, James Harold, 1896-en_US
dc.date.accessioned2009-03-16T19:56:30Z
dc.date.available2009-03-16T19:56:30Z
dc.date.issued1924en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/44890
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1924.en_US
dc.description.statementofresponsibilityby James H. Doolittle.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.titleWing loads as determined by the accelerometeren_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Aeronautical Engineering Dept.en_US
dc.identifier.oclc37379270en_US


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