Mechanism investigation and comparison of long-term deformations caused by process-induced residual stresses in thermosetting CF/epoxy and thermoplastic CF/PAEK composite laminates

This study experimentally and numerically investigated the mechanisms of process-induced deformations (PIDs) and subsequent long-term deformations (LTDs) in thermosetting CF/epoxy (T700G/2510) and thermoplastic CF/PAEK (T700G/LM-PAEK) aerospace-grade prepreg laminates. Warpage deformations in asymmetric cross-ply laminates after autoclave fabrication were measured over 84 days under controlled conditions (60 °C and 50%RH). A finite element analysis integrating anisotropic viscoelastic constitutive law and geometric nonlinearity was conducted to predict the PID and LTD using the material properties derived from the lamina-level thermomechanical analysis and dynamic mechanical analysis (DMA). The experimental results revealed that T700G/LM-PAEK exhibited a larger PID, which was attributed to its larger thermal strain and higher modulus during molding. In contrast, T700G/2510 exhibited a larger LTD, which was attributed to its higher sensitivity to moisture absorption. Although incorporating a moisture-sensitive shift factor was required for predicting the LTD of T700G/2510, the simulation accurately reproduced the PID and LTD for both materials. To validate the deformation simulation and provide insights into the viscoelastic behavior of the resin in aerospace-grade commercial prepregs with undisclosed chemical compositions, a self-consistent micromechanics model was further employed. This model estimated the equivalent viscoelastic properties of the resin from lamina-level DMA data. The findings demonstrated that both macroscale deformation prediction and microscale resin characterization can be achieved using only standard DMA tests on such prepregs. • Process-induced deformation (PID) and long-term deformation (LTD) are measured. • PID is larger in T700G/LM-PAEK (CF/PAEK); LTD is larger in T700G/2510 (CF/epoxy). • Temperature-dependent relaxation and thermal expansion explain the PID mechanism. • Moisture effects explain the LTD mechanism; T700G/LM-PAEK shows higher resistance. • Equivalent resin viscoelasticity of both prepregs is estimated using micromechanics.

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Publication Details

Journal
Composites Part A Applied Science and Manufacturing
Published
2025-05-01
DOI
https://doi.org/10.1016/j.compositesa.2025.108963
Citations
15
Primary Topic
Mechanical Behavior of Composites
Type
article
Field-Weighted Citation Impact
12.95

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article

Mechanism investigation and comparison of long-term deformations caused by process-induced residual stresses in thermosetting CF/epoxy and thermoplastic CF/PAEK composite laminates

Yoshiaki Kawagoe, Kazuki Ryuzono, Yamato Hoshikawa, Tomonaga Okabe et al.
15 citations
Composites Part A Applied Science and Manufacturing
Mechanical Behavior of Composites
12.95
article

Mechanism investigation and comparison of long-term deformations caused by process-induced residual stresses in thermosetting CF/epoxy and thermoplastic CF/PAEK composite laminates

Yoshiaki Kawagoe, Kazuki Ryuzono, Yamato Hoshikawa, Tomonaga Okabe, Sang-Wan Koo
article en
15 citations

Abstract

This study experimentally and numerically investigated the mechanisms of process-induced deformations (PIDs) and subsequent long-term deformations (LTDs) in thermosetting CF/epoxy (T700G/2510) and thermoplastic CF/PAEK (T700G/LM-PAEK) aerospace-grade prepreg laminates. Warpage deformations in asymmetric cross-ply laminates after autoclave fabrication were measured over 84 days under controlled conditions (60 °C and 50%RH). A finite element analysis integrating anisotropic viscoelastic constitutive law and geometric nonlinearity was conducted to predict the PID and LTD using the material properties derived from the lamina-level thermomechanical analysis and dynamic mechanical analysis (DMA). The experimental results revealed that T700G/LM-PAEK exhibited a larger PID, which was attributed to its larger thermal strain and higher modulus during molding. In contrast, T700G/2510 exhibited a larger LTD, which was attributed to its higher sensitivity to moisture absorption. Although incorporating a moisture-sensitive shift factor was required for predicting the LTD of T700G/2510, the simulation accurately reproduced the PID and LTD for both materials. To validate the deformation simulation and provide insights into the viscoelastic behavior of the resin in aerospace-grade commercial prepregs with undisclosed chemical compositions, a self-consistent micromechanics model was further employed. This model estimated the equivalent viscoelastic properties of the resin from lamina-level DMA data. The findings demonstrated that both macroscale deformation prediction and microscale resin characterization can be achieved using only standard DMA tests on such prepregs. • Process-induced deformation (PID) and long-term deformation (LTD) are measured. • PID is larger in T700G/LM-PAEK (CF/PAEK); LTD is larger in T700G/2510 (CF/epoxy). • Temperature-dependent relaxation and thermal expansion explain the PID mechanism. • Moisture effects explain the LTD mechanism; T700G/LM-PAEK shows higher resistance. • Equivalent resin viscoelasticity of both prepregs is estimated using micromechanics.

Composites Part A Applied Science and ManufacturingVol. 196
University of Washington (US), Tohoku University (JP), National Institute for Materials Science (JP), University of Washington Applied Physics Laboratory (US)
New Energy and Industrial Technology Development Organization, Japan Society for the Promotion of Science
Openalex Percentile: Top 1%
Mechanical Behavior of Composites
12.95
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