首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Buckling analysis of laminated composite plates submitted to compression after impact
Authors:A M Amaro  P N B Reis  M F S F de Moura  M A Neto
Institution:3. CEMUC; Department of Mechanical Engineering, University of Coimbra, Pinhal de Marrocos, 3030, Coimbra, Portugal
1. Department of Electromechanical Engineering, University of Beira Interior — UBI, 6200, Covilh?, Portugal
2. Faculty of Engineering, University of Porto, Rua Dr. Roberto Frias, 4200-465, Porto, Portugal
Abstract:The aim of this work is the experimental evaluation of the residual strength of composite laminates under compression after low velocity impact. Different kinds of delaminations, partial, embedded and through-the-width, were studied. Carbon-fibre reinforced epoxy composite was used and the experimental tests were performed on 0]16, 0, 90, 0, 90]2S and 0i, 90i]s with i=2, 3, 4, 5, using a drop-weight-testing machine. The impacted plates were inspected by the ultrasonic C-Scan to evaluate the size and the shape of the delamination. Results show that the presence of delamination decreases the compressive strength. The stacking sequence and laminate thickness were verified to have a remarkable influence on the value of the residual compressive strength, and play an important role on the observed buckling failure modes.
Keywords:
本文献已被 SpringerLink 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号