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Wing loads as determined by the accelerometer

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dc.contributor.author Doolittle, James Harold, 1896- en_US
dc.date.accessioned 2009-03-16T19:56:30Z
dc.date.available 2009-03-16T19:56:30Z
dc.date.issued 1924 en_US
dc.identifier.uri http://hdl.handle.net/1721.1/44890
dc.description Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1924. en_US
dc.description.statementofresponsibility by James H. Doolittle. en_US
dc.format.extent 1 v. in various pagings en_US
dc.language.iso eng en_US
dc.publisher Massachusetts Institute of Technology en_US
dc.rights M.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.uri http://dspace.mit.edu/handle/1721.1/7582 en_US
dc.subject Aeronautical Engineering Dept. en_US
dc.title Wing loads as determined by the accelerometer en_US
dc.type Thesis en_US
dc.description.degree M.S. en_US
dc.contributor.department Massachusetts Institute of Technology. Aeronautical Engineering Dept. en_US
dc.identifier.oclc 37379270 en_US


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