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Wing loads as determined by the accelerometer

dc.contributor.authorDoolittle, James Harold, 1896-1993.en_US
dc.date.accessioned2009-03-16T19:56:30Z
dc.date.available2009-03-16T19:56:30Z
dc.date.copyright1924en_US
dc.date.issued1924en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/44890en_US
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1924en_US
dc.description.statementofresponsibilityby James H. Doolittle.en_US
dc.format.extent1 v. in various pagingsen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.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.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautical Engineeringen_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. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc37379270en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Aeronautical Engineeringen_US
dspace.imported2022-02-10T17:30:50Zen_US


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