Failure mode estimation at highly loaded thick composite lugs representing rotary wing UAS blade root
Failure mode estimation at highly loaded thick composite lugs representing rotary wing UAS blade root
| dc.contributor.author | Tursun, G. | |
| dc.contributor.author | Maradit, B.P. | |
| dc.contributor.author | Taskinoglu, E. | |
| dc.date.accessioned | 2016-07-01T12:58:53Z | |
| dc.date.available | 2016-07-01T12:58:53Z | |
| dc.date.issued | 2011 | |
| dc.identifier.other | ERF 2011_198 | |
| dc.identifier.uri | http://hdl.handle.net/20.500.11881/850 | |
| dc.language.iso | en | |
| dc.title | Failure mode estimation at highly loaded thick composite lugs representing rotary wing UAS blade root |
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