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   Progressive Damage Analysis of Laminated Composites using Continuum Damage Mechanics  
   
نویسنده Moliammadi B. ,Hosseini-Toudesliky H. ,Sadr M. H.
منبع journal of aerospace science and technology - 2009 - دوره : 6 - شماره : 2 - صفحه:99 -113
چکیده    In this paper, progressive damage and global failure of composite laminates under quasi-static, monotonia loading are investigated using 3d continuum damage mechanics. for this purpose, a finite element program has been developed using an eight-node 2d layered element, including layer-wise plate theory. damage analysis of a single orthotropic layer under various uniform in-plane and transverse loading conditions, and laminate problems with diffuse damage under simply supported and distributed transverse loading conditions are performed. the effects of modeling parameters such as hardening rule:s and mesh densities along the laminate thickness and in-plane surface on the progressive damage response and global failure are also investigated.
آدرس iran university of science and technology, School of Mech Eng , ایران, amirkabir university of technology, Dept of Aerospace Eng , ایران, amirkabir university of technology, Dept of Aerospace Eng , ایران
پست الکترونیکی ilosseini&aut.ac.'tr.
 
     
   
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