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dc.contributor.advisorOtto C. Koppen.
dc.contributor.authorShumowsky, Stanislaw A. (Stanislaw Anton)en_US
dc.date.accessioned2024-04-30T23:57:44Z
dc.date.available2024-04-30T23:57:44Z
dc.date.copyright1936en_US
dc.date.issued1936en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/154353
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1936en_US
dc.descriptionIncludes bibliographical references (leaves 68-70).en_US
dc.description.statementofresponsibilityby Stanislaw A. Shumowsky.en_US
dc.format.extent100 leaves (some folded)en_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.titleThe efficiency of the vertical tail for different wing-fuselage combinations, particularly at high angles of attacken_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc35515657en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Aeronautical Engineeringen_US
dspace.imported2024-04-30T23:57:44Zen_US
mit.thesis.degreeMasteren_US


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