ID 1085

New Progress on Prediction Methodology for

Residual Strength of Damaged Composite Laminates in ASRI

Zhen SHEN*, Puhui CHEN*, Xiaodong TANG**, Yanan CHAI* and Feng LIU *

* Aircraft Strength Research Institute, Xi’an, 710065, CHINA

** Aerospace Eng. Dept., Texas A & M University, TX77843-3141, USA

Keywords: composite laminates, damage, residual strength, failure criteria, stiffened panels