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An experimental investigation of the minimum Reynolds' number for instability in water jets

Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1960. / MIT copy bound with: Nonlinear control system for the control of yaw angle of an aircraft / Jason L. Speyer. 1960. / Includes bibliographical references (leaf 14). / by Andrus Viilu. / B.S.

Identiferoai:union.ndltd.org:MIT/oai:dspace.mit.edu:1721.1/113189
Date January 1960
CreatorsViilu, Andrus
ContributorsErik Mollo-Christensen., Massachusetts Institute of Technology. Aeronautical Engineering Department., Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
PublisherMassachusetts Institute of Technology
Source SetsM.I.T. Theses and Dissertation
LanguageEnglish
Detected LanguageEnglish
TypeThesis
Format14, A7 leaves, 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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