Volume 22 Issue 5
May  2007
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Article Navigation >  Journal of Aerospace Power  > 2007  >  22(5): 749-754
WEN Wei-dong, CUI Hai-po, XU Ying. Research on impact damage of T300/BMP-316 composite laminates[J]. Journal of Aerospace Power, 2007, 22(5): 749-754.
Citation: WEN Wei-dong, CUI Hai-po, XU Ying. Research on impact damage of T300/BMP-316 composite laminates[J]. Journal of Aerospace Power, 2007, 22(5): 749-754.
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Research on impact damage of T300/BMP-316 composite laminates

  • College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

  • Received Date: 2005-05-10
  • Rev Recd Date: 2006-08-21
  • Publish Date: 2007-05-28
    Abstract
  • The experimental research of low speed impact damage has been carried out on composite laminates with different geometries and layer direction angle,and the impact process was simulated by the progressive damage method.The geometries of composite laminates have much effect on the impact damage projected area.The layer direction angle of composite laminates has little effect on the impact damage projected area,but it has influence on the impact damage figure.

     

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