The Static Strength Reliability Analysis of Composite Aircraft Structures

被引：1
|
作者：
Lin, Longxiang [1 ]
Mou, Haolei [2 ]
Ren, Jian [2 ]
Zou, Tianchun [2 ]
机构：
[1] Air China Tech, Beijing 101312, Peoples R China
[2] Civil Aviat Univ China, Key Lab Civil Aircraft Airworthinesa & Maintenanc, Tianjin 300300, Peoples R China
来源：
MATERIALS SCIENCE, CIVIL ENGINEERING AND ARCHITECTURE SCIENCE, MECHANICAL ENGINEERING AND MANUFACTURING TECHNOLOGY, PTS 1 AND 2 | 2014年 / 488-489卷
关键词：
Composite; Aircraft Structure; Static Strength; Reliability Analysis;
D O I：
10.4028/www.scientific.net/AMM.488-489.1215
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
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.
引用
收藏
页码：1215 / +
页数：2
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