Thick Composite Plates Subjected to Lateral Loading
Author:
Affiliation:
1. Technology Laboratory for Advanced Composites, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/54/3/611/5459893/611_1.pdf
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3. Predictive model for the spherical indentation of composite laminates with finite thickness;Composite Structures;2016-10
4. Comparison of Delamination Threshold Load Prediction on Low Velocity Impact of Composite Panels with Different Thickness;56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2015-01-02
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