The evolution of thermal residual stresses induced during curing processing has been investigated. A micro-mechanical model of a cross-ply laminates is analyzed using viscoelastic finite element method. The polymer matrix is represented by a non-linear viscoelastic constitutive model. To study possible bounds of the residual stresses two types of analyses were carried out: one with temperature-independent and the other with temperature-dependent material constants. The results indicate that a higher cooling rate results in higher residual stresses in the laminates. However, due to the viscosity of the polymer matrix, the residual stresses relax with time and tend to an asymptotic small value irrespective of the different cooling rates. The average shrinkage strains and the coefficients of thermal expansion (CTE) of the composites, correspondingly, are also time-dependent and approach an asymptotic value after the stress relaxation process.
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ASME 2002 Pressure Vessels and Piping Conference
August 5–9, 2002
Vancouver, BC, Canada
Conference Sponsors:
- Pressure Vessels and Piping Division
ISBN:
0-7918-4654-7
PROCEEDINGS PAPER
Thermal Residual Stresses Induced During Manufacturing Process of Fiber Reinforced Polymeric Composites
Zihui Xia,
Zihui Xia
University of Alberta, Edmonton, Alberta, Canada
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Yunfa Zhang,
Yunfa Zhang
University of Alberta, Edmonton, Alberta, Canada
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Fernand Ellyin
Fernand Ellyin
University of Alberta, Edmonton, Alberta, Canada
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Zihui Xia
University of Alberta, Edmonton, Alberta, Canada
Yunfa Zhang
University of Alberta, Edmonton, Alberta, Canada
Fernand Ellyin
University of Alberta, Edmonton, Alberta, Canada
Paper No:
PVP2002-1365, pp. 171-175; 5 pages
Published Online:
August 14, 2008
Citation
Xia, Z, Zhang, Y, & Ellyin, F. "Thermal Residual Stresses Induced During Manufacturing Process of Fiber Reinforced Polymeric Composites." Proceedings of the ASME 2002 Pressure Vessels and Piping Conference. Fatigue, Fracture and Damage Analysis, Volume 2. Vancouver, BC, Canada. August 5–9, 2002. pp. 171-175. ASME. https://doi.org/10.1115/PVP2002-1365
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