...统计学与断裂力学的基础,利用已有的飞机单细节结构试验结果,提出一种定量计算飞机结构发生多部位损伤(MSD,Multiple Site Damage)可能性的方法.该方法简化了飞机结构发生MSD可能性的计算,为飞机结构的安全性评估提供基础.
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In this dissertation, the stress intensity factors and the residual strength of panels with multiple site damage are studied in detail.
本文主要研究了含多部位损伤结构的应力强度因子和剩余强度。
An analytical and experimental study were performed on the fatigue crack growth of stiffened LY12CZ Aluminum Alloy panels with multiple site damage (MSD).
进行了多处损伤LY 12 CZ铝合金加筋板的疲劳裂纹扩展的分析与试验研究。
Multiple Site Damage (MSD) is one of important factors which affect structural completeness of old aircraft.
多处损伤（MSD）是影响老龄飞机结构完整性的重要因素之一。
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