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A stress-continuous laminate theory for composites and sandwich structures

  • Bing Qi Si
  • , Yi Hong*
  • , Miao Miao Li
  • , Shi Jun Qu
  • , Ji Yuan Liu
  • , Xiao Dong He
  • *Corresponding author for this work
  • Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

This paper proposes a new Equivalent Single Layer (ESL) theory, termed the Higher-order Laminate Theory with A-Priori Stress Continuity (HLT-APSC). Starting from an assumed transverse stress field, HLT-APSC inherently ensures that the derived displacement functions satisfy the C° continuity conditions for transverse displacements and stresses. This approach yields higher accuracy than traditional ESL theories in predicting both the bending deformations of thick plates and higher-order vibration modes. The governing equations and boundary conditions for free vibration are derived within the HLT-APSC framework. The accuracy of HLT-APSC is evaluated through four laminated / sandwich beam case studies. Validated against reference solutions, the proposed HLT-APSC yields natural frequency errors of 3.125%, 12.85%, and 10.00% for the first three cases, respectively. In comparison, the traditional Third-order Shear Deformation Theory (TSDT) results in errors of 3.125%, 14.02%, and 54.98%. For the fourth example, the predicted error is merely 1.182%. Furthermore, HLT-APSC is capable of capturing the C° continuity of transverse shear and normal stresses. The proposed HLT-APSC offers a new perspective for enhancing the predictive accuracy of ESL theories. Despite its current limitations, the HLT-APSC is expected to contribute to more efficient and accurate modeling of relatively thick composite laminates and sandwich structures with soft cores.

Original languageEnglish
Article number111508
JournalInternational Journal of Mechanical Sciences
Volume318
DOIs
StatePublished - 15 May 2026

Keywords

  • Composite laminate
  • Equivalent single layer theory
  • Free vibration
  • Higher-order laminate theory
  • Sandwich structure
  • Transverse stress

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