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Zhang Long, Liao Wenlin, Chen Xiaoguang, et al. Multi-scale simulation and test verification for the high-temperature compression behavior of corrugated lattice sandwich panel[J]. Journal of Aerospace Power, 2026, 42(X):20250296 doi: 10.13224/j.cnki.jasp.20250296
Citation: Zhang Long, Liao Wenlin, Chen Xiaoguang, et al. Multi-scale simulation and test verification for the high-temperature compression behavior of corrugated lattice sandwich panel[J]. Journal of Aerospace Power, 2026, 42(X):20250296 doi: 10.13224/j.cnki.jasp.20250296

Multi-scale simulation and test verification for the high-temperature compression behavior of corrugated lattice sandwich panel

doi: 10.13224/j.cnki.jasp.20250296
  • Received Date: 2025-06-20
    Available Online: 2026-09-30
  • In order to master the macroscopic mechanical response rules of the integrated thermal insulation and load bearing lattice sandwich panel structure of hypersonic aircraft, this paper carried out multi-scale simulation and test verification of the high-temperature compression behavior of corrugated lattice sandwich panels. First, the basic theory of general method of cells (GMC) is introduced. Then, on the basis of the periodic structural characteristics of corrugated lattice sandwich panels, the representative volume element is extracted to carry out multi-scale simulation and macroscopic effective mechanical parameters prediction based on the GMC method. In the end, a high-temperature compression test is designed to verify this developed method. It shows that the macroscopic stress strain curve and interior mesoscopic stress distribution predicted by this method are basically consistent with the test results, and the maximum relative error between the predicted elastic modulus and the test results is within 5.0%.

     

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