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dc.contributor.authorKlemin, Alexander,1888-1950.en_US
dc.date.accessioned2019-07-23T19:53:39Z
dc.date.available2019-07-23T19:53:39Z
dc.date.copyright1916en_US
dc.date.issued1916en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/121931
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1916.en_US
dc.description.statementofresponsibilityby Alexander Klemin.en_US
dc.format.extent6, [11] leavesen_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.titleMathematical development of and tests on propeller sections of varying thicknessen_US
dc.typeThesisen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc38055248en_US
dc.description.collectionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1916.en_US
dspace.imported2019-07-23T19:53:37Zen_US
mit.thesis.degreeMasteren_US
mit.thesis.departmentAeroen_US


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