| Autor: |
Lin, Long Xiang, Mou, Hao Lei, Ren, Jian, Zou, Tian Chun |
| Zdroj: |
Applied Mechanics and Materials; January 2014, Vol. 488 Issue: 1 p1215-1218, 4p |
| Abstrakt: |
The static strength design of aircraft structure is the most basic design principles. The basic applicable conditions of composite structures static strength reliability analysis using the current methods were mentioned in this paper, and compliance analysis of these basic conditions was carried out. In addition, further studies were also conducted to research the influence of the number of full-scale structural specimens and environmental factors on the composite structures static strength reliability. |
| Databáze: |
Supplemental Index |
| Externí odkaz: |
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