• Title of article

    Effect of SACMA and QMW Test Methods on Compressive Properties of Composite Laminates after Low Velocity Impact

  • Author/Authors

    CHENG، نويسنده , , Xiao-Quan and Zhang، نويسنده , , Zi-long and YI، نويسنده , , Xiaosu and Wu، نويسنده , , Xue-ren، نويسنده ,

  • Issue Information
    روزنامه با شماره پیاپی سال 2002
  • Pages
    8
  • From page
    90
  • To page
    97
  • Abstract
    Experimental studies on the compressive behavior of composite laminates after low velocity impact was carried out with two test methods. One is SACMA Standard, and the other is a small dimensional specimen test method. Impact damage distributions, compressive failure process after impact, quasi-static indentation and compression of laminates with a hole were brought into comparison between these two test methods. The results showed that there is a great difference between these two test methods. Compressive behavior of laminates after impact varies with different test methods. Residual compressive strength of laminates after low velocity impact measured with SACMA Standard can reflect stiffness properties of composite resins more wholely than that measured with the other method can do. Small dimensional specimen test method should be improved on as an experimental standard of compressive strength after impact.
  • Keywords
    Low Velocity Impact , Composite laminates , Damage , Residual compressive strength , Test methods
  • Journal title
    Chinese Journal of Aeronautics
  • Serial Year
    2002
  • Journal title
    Chinese Journal of Aeronautics
  • Record number

    2264387