Figures index

From

Analysis of Sandwich Structures by the FEM

Peter Sivák, Ingrid Delyová, Patrícia Diabelková

American Journal of Mechanical Engineering. 2017, 5(6), 243-246 doi:10.12691/ajme-5-6-2
  • Figure 1. Basic schematic view of sandwich structure [2]
  • Figure 2. Similarity of “I” profile and the multilayer sandwich structure [8]
  • Figure 3. The characteristic distribution of stress in cross-section during the loading process [8]
  • Figure 4. FEM model of honeycomb
  • Figure 5. The cross-linked honeycomb model
  • Figure 6. Maximal stress of honeycomb with the core height v = 20 mm
  • Figure 7. The fold of the honeycomb with the core height v = 20 mm
  • Figure 8. Dependence of maximal stress σmax to the core height (the aluminium alloy and the carbon steel)
  • Figure 9. Dependence of height of fold to core height (the aluminium alloy and the carbon steel)
  • Figure 10. Dependence of maximal stress σmax to the core height (the copper and the carbon steel)
  • Figure 11. Dependence of fold to core height (the copper and the carbon steel)
  • Figure 12. Dependence of maximal stress σmax to the core height (the titanium and the carbon steel)
  • Figure 13. Dependence of fold to core height (the titanium and the carbon steel)