| dc.contributor.author |
Doolittle, James Harold, 1896- |
en_US |
| dc.date.accessioned |
2009-03-16T19:56:30Z |
|
| dc.date.available |
2009-03-16T19:56:30Z |
|
| dc.date.issued |
1924 |
en_US |
| dc.identifier.uri |
http://hdl.handle.net/1721.1/44890 |
|
| dc.description |
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1924. |
en_US |
| dc.description.statementofresponsibility |
by James H. Doolittle. |
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 |
Wing loads as determined by the accelerometer |
en_US |
| dc.type |
Thesis |
en_US |
| dc.description.degree |
M.S. |
en_US |
| dc.contributor.department |
Massachusetts Institute of Technology. Aeronautical Engineering Dept. |
en_US |
| dc.identifier.oclc |
37379270 |
en_US |
