节点文献
耐久性分析技术的发展与改进
DEVELOPMENT AND IMPROVEMENT OF DURABILITY ANALYSIS TECHNIQUE
【摘要】 阐述了美国空军耐久性设计手册(第二版)所做的发展,并指出其中存在的两个问题,即确定裂纹扩展率参数Q时未考虑裂纹萌生时间的重要作用和没有说明使用期裂纹扩展率标准差σz的确定方法.通过研究,改进了裂纹扩展率参数Q的确定方法,补充了确定裂纹扩展率标准差σz的途径.并通过了实例验证.
【Abstract】 This thesis introduces the method developed by USAF durability design homdbook Ⅱ.There are two problems in it. One is that the important of time of crack initiation isn’t considered while calculating crack growth rate parameter Q. Another is that the determination of the standard deviation σz of crack growth rate is not given. In this researching. the method of calculating paprameter Q is improved and the approach of determining standard deviation σz is given. A last. the methods are tested by a practical example.
【关键词】 耐用性;
飞机;
结构设计;
裂纹扩展;
偏差;
【Key words】 durability; airplanes; structural design; crack propagation; deviations;
【Key words】 durability; airplanes; structural design; crack propagation; deviations;
- 【文献出处】 北京航空航天大学学报 ,JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS , 编辑部邮箱 ,1995年01期
- 【分类号】V215.6
- 【被引频次】9
- 【下载频次】159