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Buckling analysis of delaminated composite plates using a novel layerwise theory
Affiliation:1. Mechanical Engineering Department, Sahand University of Technology, Sahand New Town, Tabriz, Azerbayjan Sharghi, Iran;2. Aerospace Engineering Department and the Center of Excellence in Computational Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran;1. Institute of General Mechanics, RWTH Aachen University, Templergraben 64, D-52062 Aachen, Germany;2. School of Mechanical Engineering, Northwestern Polytechnical University, 710072 Xi''an, PR China;1. College of Information Science and Technology, Shanghai Ocean University, Shanghai 201306, China;2. Department of Architecture and Civil Engineering, City University of Hong Kong, Kowloon, Hong Kong Special Administrative Region;3. City University of Hong Kong Shenzhen Research Institute Building, Shenzhen Hi-Tech Industrial Park, Nanshan District, Shenzhen, China;1. College of Mechanics and Materials, Hohai University, 210098 Nanjing, China;1. German Aerospace Center (DLR), Lilienthalplatz 7, D-38108 Braunschweig, Germany;2. Nanyang Technological University (Graduate Student), 50 Nanyang Avenue, Singapore 639798, Singapore
Abstract:
Keywords:Buckling  Layerwise theory  Delamination  Composite plates  First order shear deformation theory
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