A dynamic nonlinear model of multilayered composite shells featuring damaged interfaces
Author:
Affiliation:
1. Torino, Politecnico, Turin, Italy
2. Virginia Polytechnic Inst. and State Univ., Blacksburg
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1384
Reference16 articles.
1. Vibration of geometrically imperfect panels subjected to thermal and mechanical loads
2. Frequency-load interaction of geometrically imperfect curved panels subjected to heating
3. An Improved Shear-Deformation Theory for Moderately Thick Multilayered Anisotropic Shells and Plates
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1. Generalized layerwise mechanics for the static and modal response of delaminated composite beams with active piezoelectric sensors;International Journal of Solids and Structures;2007-12
2. Layerwise Dynamic Response Models for Delamination Composite Beams with Active Piezoelectric Sensors;46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2005-04-18
3. A global/local third-order Hermitian displacement field with damaged interfaces and transverse extensibility: analytical formulation;Composite Structures;2003-03
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