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Wing loads as determined by the accelerometer

Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1924 / by James H. Doolittle. / M.S. / M.S. Massachusetts Institute of Technology, Department of Aeronautical Engineering

Identiferoai:union.ndltd.org:MIT/oai:dspace.mit.edu:1721.1/44890
Date January 1924
CreatorsDoolittle, James Harold, 1896-1993.
ContributorsMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
PublisherMassachusetts Institute of Technology
Source SetsM.I.T. Theses and Dissertation
Detected LanguageEnglish
TypeThesis
Format1 v. in various pagings, application/pdf
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., http://dspace.mit.edu/handle/1721.1/7582

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