Finite element analysis of hypervelocity impact behaviour of cfrp-al/hc sandwich panel

HIGHLIGHTS

  • who: Phadnis Vaibhav A. and Silberschmidt Vadim V. from the AMRC with Boeing, The University of Sheffield, UK have published the article: Finite element analysis of hypervelocity impact behaviour of CFRP-Al/HC sandwich panel, in the Journal: (JOURNAL)
  • how: The following criteria were proposed to model failure in the σ22 qs K (˙ )X 2t σ12 qs K (γ̇ )S12 σ23 qs K (γ̇ )S23 2 ≥ 1 σ22 + σ33 > 0 dmt=1... (tensile failure) σ22 + σ33 and amplt 0 dmc=1... (compressive failure).

SUMMARY

    Advanced composite materials such as CFRP/Al-HC (carbon . . .

     

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