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Investigation of laminated composite plates under impact dynamic loading using a three-dimensional hybrid stress finite element method

โœ Scribed by C.T. Sun; W.J. Liou


Publisher
Elsevier Science
Year
1989
Tongue
English
Weight
612 KB
Volume
33
Category
Article
ISSN
0045-7949

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An assumed hybrid-stress finite element model incorporating two types of modified composite multilayer elements (MLTUP and MLTPH) is developed to investigate the free vibration of doubly and singly patched cracked laminates. Three-dimensional stresses of the laminated panel, patch and adhesive are a