Micromechanics Modeling of Long-Term Interlaminar Properties of Woven Fabric Polymer Composites
Abstract
The objective of the paper is to study the longterm interlaminar properties in woven fabric polymer composites using micromechanical models. Characterization of the viscoelastic behavior of a five harness satin woven-fiber cross-ply composite laminate is presented, taking into consideration the weave architecture and time-dependent effects. The classical lamination theory model proposed by Raju and Wang is adapted to include the in-plane elastic behavior of woven fiber composites. For the matrix-dominated out-of-plane response, a viscoelastic creep model is developed based on Schapery's nonlinear viscoelastic constitutive law. In addition, physical aging of the matrix has been included in the model using the effective time theory proposed by Struik. Furthermore, the time dependent out-of-plane behavior is predicted using a two-dimensional micro-mechanical model.
Recommended Citation
V. Gupta et al., "Micromechanics Modeling of Long-Term Interlaminar Properties of Woven Fabric Polymer Composites," Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, American Institute of Aeronautics and Astronautics (AIAA), Jan 2001.
The definitive version is available at https://doi.org/10.2514/6.2001-1282
Meeting Name
Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2001, Seattle, WA)
Department(s)
Mechanical and Aerospace Engineering
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2001 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
01 Jan 2001