제목 | A study on the Prediction Model of Residual Strength after impact in Aircraft Composites | ||||
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작성자 | 건전성평가연구실 | 등록일 | 2015-10-23 | 조회수 | 570 |
J.H. Choi, M. S. Kang, H.S. Park, J.M. Koo, C.S. Seok
A study on the Prediction Model of Residual Strength after impact in Aircraft Composites The Eighteenth Annual International Conference on Composite/Nano Engineering (ICCE-18) Ancorage, USA July, 4-10, 2010 |
이전글 | A Study on Fracture toughness of nuclear piping material by various types of specimen |
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다음글 | Fatigue life Prediction of Woven CFRP |