Modeling the Residual Stress in Woven Thermoset Composites Parts for Aerospace Applications Using Finite Element Methods
Process induced residual stresses in thermoset composite parts is one of significant issue faced by the industry. Its Modelling is a coupled multiphysics phenomena. Precise information about the chemical shrinkage, thermal expansion coefficient, cure kinetics, heat transfer and constitutive equation...
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| Veröffentlicht in: | Advanced Materials Research 2015-04, Vol.1099, p.32-36 |
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| creator | Beauchêne, Pierre Saouab, Abdelghani Agogué, Romain Nawab, Yasir Park, Chung Hae |
| description | Process induced residual stresses in thermoset composite parts is one of significant issue faced by the industry. Its Modelling is a coupled multiphysics phenomena. Precise information about the chemical shrinkage, thermal expansion coefficient, cure kinetics, heat transfer and constitutive equation are required for an accurate simulation. In this article, spring-in angle induced in woven carbon/epoxy composite bracket is modelled by solving the thermo-kinetics and thermo-mechanics coupling simultaneously in a commercial finite element software. The obtained values of spring-in angle using numerical simulation are compared with those found in the literature and both are found in agreement. |
| doi_str_mv | 10.4028/www.scientific.net/AMR.1099.32 |
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| source | Scientific.net Journals |
| subjects | Aircraft components Computer simulation Engineering Sciences Mathematical analysis Mathematical models Polymer matrix composites Residual stress Thermal expansion Thermosetting resins |
| title | Modeling the Residual Stress in Woven Thermoset Composites Parts for Aerospace Applications Using Finite Element Methods |
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