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Carbon Fiber Reinforced Polymer (CFRP) composites are well established in aircraft, aerospace and automotive industry due to their lightweight structure and robustness. Generally, in uni-directional (UD) composite laminates the mechanical properties depend of fiber orientation, the number and the thickness of the plies and the stacking sequence [1], Fig. 1. In continuous fiber laminates the prediction of failure is dependent on the fiber orientation and the failure criteria that are adopted.

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Low Velocity Impact (LVI) Simulation of a CFRP Ply-Drop Laminates: A Numerical Analysis

  • 会议论文

  • 发表日期：

    2025年

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  • Mario Russo,
  • Evanthia Pappa,
  • A. Baroni,
  • S. Corvaglia,
  • Valentina Lopresto,
  • Ilaria Papa

摘要

Carbon Fiber Reinforced Polymer (CFRP) composites are well established in aircraft, aerospace and automotive industry due to their lightweight structure and robustness. Generally, in uni-directional (UD) composite laminates the mechanical properties depend of fiber orientation, the number and the thickness of the plies and the stacking sequence [1], Fig. 1. In continuous fiber laminates the prediction of failure is dependent on the fiber orientation and the failure criteria that are adopted.