dc.contributor.author | Klemin, Alexander,1888-1950. | en_US |
dc.date.accessioned | 2019-07-23T19:53:39Z | |
dc.date.available | 2019-07-23T19:53:39Z | |
dc.date.copyright | 1916 | en_US |
dc.date.issued | 1916 | en_US |
dc.identifier.uri | https://hdl.handle.net/1721.1/121931 | |
dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1916. | en_US |
dc.description.statementofresponsibility | by Alexander Klemin. | en_US |
dc.format.extent | 6, [11] leaves | en_US |
dc.publisher | Massachusetts Institute of Technology | en_US |
dc.rights | MIT 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.uri | http://dspace.mit.edu/handle/1721.1/7582 | en_US |
dc.title | Mathematical development of and tests on propeller sections of varying thickness | en_US |
dc.type | Thesis | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
dc.identifier.oclc | 38055248 | en_US |
dc.description.collection | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1916. | en_US |
dspace.imported | 2019-07-23T19:53:37Z | en_US |
mit.thesis.degree | Master | en_US |
mit.thesis.department | Aero | en_US |