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Volume 38 Issue 7
Jul.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (7): 947-952.
Chai Xue, Wang Ganglin, Wu Zheet al. Aileron control and reconfiguration of flying wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(12): 1511-1515. (in Chinese)
Citation: Qi Zhongxin, Yan Ying, Liu Yujia, et al. Hygrothermal properties simulation and damage analysis of T300/QY8911 undirectional laminates[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (7): 947-952. (in Chinese)
shu

Hygrothermal properties simulation and damage analysis of T300/QY8911 undirectional laminates

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 14 Apr 2011
  • Publish Date: 30 Jul 2012
    Abstract
  • Flexural properties of T300/QY8911 undirectional laminates were tested under different hygrothermal conditions. Finite element models of composite undirectional laminates under hygrothermal conditions were built. The flexural properties of T300/QY8911 undirectional laminates tested in experimentation were simulated. Plus, a damage evolution simulation module of composite was developed. The integrated damage evolution process of T300/QY8911 undirectional laminates under hygrothermal conditions was simulated. Results show that, the flexural modulus of T300/QY8911 undirectional laminates remains unchanged under different hygrothermal conditions, but the flexural strength changes greatly with conditions. For flexural modulus, the error between simulation values and test results is less than 6%, and for flexural strength, it is less than 2%. The finite element models can predict flexural properties of composite undirectional laminates under different hygrothermal conditions relative exactly.

     

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    • References(13)
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