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dc.contributor.authorKendall, Delvin E.en_US
dc.contributor.authorWhitcomb, David W.en_US
dc.date.accessioned2024-05-21T20:57:41Z
dc.date.available2024-05-21T20:57:41Z
dc.date.copyright1945en_US
dc.date.issued1945en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/155022
dc.descriptionThesis: M.S., Massachusetts Institute of Technology, Department of Electrical Engineering, 1945en_US
dc.descriptionBibliography: leaves 115-117.en_US
dc.description.statementofresponsibilityby Delvin E. Kendall, Jr. and David W. Whitcomb.en_US
dc.format.extent117 leavesen_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.subjectElectrical Engineeringen_US
dc.titleDevelopment of an automatic sideslip control for aircraft,en_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Electrical Engineeringen_US
dc.identifier.oclc26660845en_US
dc.description.collectionM.S. Massachusetts Institute of Technology, Department of Electrical Engineeringen_US
dspace.imported2024-05-21T20:57:41Zen_US
mit.thesis.degreeMasteren_US


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