宇航材料工艺2011，Vol.41Issue(3)：20-26,7.
含损伤复合材料层合板剩余压缩强度研究进展
Advance of Study on Residual Compressive Strength of Damaged Composite Laminates
摘要
Abstract
Advances in damage analysis for composite laminates are summarized. Emphasis is placed on the residual compressive strength of the damaged composite laminates after low velocity impact in composite engineering structures. The contents of Lhe article are as follows : ( 1) damage characteristic of laminates compressive failure. (2) laminates compressive experimentation. ( 3 ) damage model analysis and failure analysis. (4) perspective for developing new analysis methods.关键词
复合材料层合板/剩余压缩强度/损伤/进展Key words
Composite laminates / Residual compressive strength/ Damage / Advance引用本文复制引用
郑锡涛,李泽江,李光亮..含损伤复合材料层合板剩余压缩强度研究进展[J].宇航材料工艺,2011,41(3):20-26,7.基金项目
国家自然科学基金项目(10872167) （10872167）
