Original Article
  • Residual Deformation Analysis of Composite by 3-D Viscoelastic Model Considering Mold Effect

  • Hong-Jun Lee*, Wie-Dae Kim*†

  • Aircraft Structural Design Lab, Department of Aerospace Engineering, Pusan National University

  • 3-D 점탄성 모델을 이용한 복합재 성형후 잔류변형해석 및 몰드 효과 연구

  • 이홍준* · 김위대*†

  • This article is an open access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/4.0) which permits unrestricted non-commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.

References
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  • 2. Choi, E.S., and Kim, W.D., “Thermal Deformation of Carbon Fiber Reinforced Composite by Cure Shrinkage,” Journal of the Korean Society for Composite Materials, Vol. 31, No. 6, 2018, pp. 404-411.
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  • 10. Seong, D.Y., and Kim, W.D., “Thermal Deformation Analysis of L-shaped Composite During Cure Process by Viscoelastic Model,” Journal of the Korean Society for Composite Materials, Vol. 33, No. 4, 2020, pp. 220-227.
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This Article

Correspondence to

  • Wie-Dae Kim

  • Aircraft Structural Design Lab, Department of Aerospace Engineering, Pusan National University

  • E-mail: wdkim@pusan.ac.kr