| dc.contributor.advisor | Erik Mollo-Christensen. | en_US |
| dc.contributor.author | Viilu, Andrus | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Aeronautical Engineering Department. | |
| dc.date.accessioned | 2018-01-12T21:16:31Z | |
| dc.date.available | 2018-01-12T21:16:31Z | |
| dc.date.issued | 1960 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/113189 | |
| dc.description | Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1960. | en_US |
| dc.description | MIT copy bound with: Nonlinear control system for the control of yaw angle of an aircraft / Jason L. Speyer. 1960. | en_US |
| dc.description | Includes bibliographical references (leaf 14). | en_US |
| dc.description.statementofresponsibility | by Andrus Viilu. | en_US |
| dc.format.extent | 14, A7 leaves | en_US |
| dc.language.iso | eng | en_US |
| dc.publisher | Massachusetts Institute of Technology | en_US |
| dc.rights | MIT 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.uri | http://dspace.mit.edu/handle/1721.1/7582 | en_US |
| dc.subject | Aeronautical Engineering Dept. | en_US |
| dc.title | An experimental investigation of the minimum Reynolds' number for instability in water jets | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | B.S. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 32933930 | en_US |
