| dc.contributor.advisor | R. H. Miller. | en_US |
| dc.contributor.author | Mallen, Joseph | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Aeronautical Engineering Department. | |
| dc.date.accessioned | 2011-11-18T20:50:06Z | |
| dc.date.available | 2011-11-18T20:50:06Z | |
| dc.date.issued | 1949 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/67130 | |
| dc.description | Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1949. | en_US |
| dc.description | Includes bibliographies. | en_US |
| dc.description.statementofresponsibility | by Joseph Mallen. | en_US |
| dc.format.extent | 1 v. in various pagings | en_US |
| dc.language.iso | eng | en_US |
| dc.publisher | Massachusetts Institute of Technology | en_US |
| dc.rights | M.I.T. theses are protected by
copyright. They may be viewed from this source for any purpose, but
reproduction or distribution in any format is prohibited without written
permission. See provided URL for inquiries about permission. | en_US |
| dc.rights.uri | http://dspace.mit.edu/handle/1721.1/7582 | en_US |
| dc.subject | Aeronautical Engineering Dept. | en_US |
| dc.title | Experimental investigation of the transient response in pitch of a helicopter | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | M.S. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 29456305 | en_US |
