Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Study on Hole Edge Stress Concentration of Composite Plate
Affiliation:

AVIC THE FIRST AIRCRAFT INSTITUTE,AVIC THE FIRST AIRCRAFT INSTITUTE,The first Aircraft Institute

Clc Number:

20120130001

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    Abstract:

    The hole stress concentration of composite plate is studied by FE method for designing the composite mechanical connections. The relations between the stress concentration and the d/B、H/d is concluded in the paper: (1) The relative width d/B and relative edge distance H/d have a great effect of stress concentration. (2) The maximum circumferential concentration factor decreases with the increase of H/d, but ratio of maximum radial stresses to bearing stress almost has no change. (3) The ratio of maximum circumferential stress to bearing stress increase with the decrease of B. As d/B changes, the Krd almost has no change, but the radial stress changed visibly. These results can be referred to design composite mechanical joint.

    Reference
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    [6]. 姚学诗. 带圆孔复合材料层合板应力集中系数的研究[J].韶关学院学报,2003,24(12):45-47Yao Xueshi. The Study on the Stress Concentration Coefficient of the Composite Laminates with a Circle Hole [J]. Journal of Shaoguan University, 2003, 24(12):45-47
    [7]. 李成,郑艳萍,吴晓玲,孟令启. 结构链接区开口正交各向异性板的应力仿真分析[J].机械设计与研究,2007,第23卷(2):06-07Li Cheng, Zheng Yanping, Wu Xiaoling, Meng Lingqi. Stress Simulation Analysis of Orthotropic Plate with Opening in Structural Connection Section [J].Machine Design and Research. 2007,23(2):06-07
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zhengjie, Li Longbin, qianchao. Study on Hole Edge Stress Concentration of Composite Plate[J]. Advances in Aeronautical Science and Engineering,2012,3(4):

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History
  • Received:January 30,2012
  • Revised:March 15,2012
  • Adopted:March 26,2012
  • Online: December 20,2012
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