Volume 29 Issue 11
Nov.  2003
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Cheng Xiaoquan, Zhao Long, Zhang Yininget al. Properties of stitched composite laminates——the principle properties of simple laminates[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(11): 1001-1005. (in Chinese)
Citation: Cheng Xiaoquan, Zhao Long, Zhang Yininget al. Properties of stitched composite laminates——the principle properties of simple laminates[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(11): 1001-1005. (in Chinese)

Properties of stitched composite laminates——the principle properties of simple laminates

  • Received Date: 25 Jun 2003
  • Publish Date: 30 Nov 2003
  • In order to solve the application of stitched composites in aircraft structures, experimental studies were carried out on the effect of stitching and stitching directions on tensile and compressive properties of unidirectional laminates and cross-ply symmetric laminates made of uniweave T300/QY9512. Some principle properties of uniweave T300/QY9512 were measured. It shows that stitching and stitching directions have little effect on the modulus of this two kind of laminates, while the effect is great on Possion ratio. The transform of off-axial modulus is not fit for Poisson ratio of off-axial stitched unidirectional laminates. Stitching and its directions have great effect on tensile strength of unidirectional laminates, but are not obvious on their compressive strength. Because the tension failure mechanisms of stitched cross-ply symmetric laminates are different from that of stitched unidirectional laminates, the strength of stitched unidirectional laminates cannot be used as the laminar strength of stitched cross-ply symmetric laminates.

     

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  • [1] Davis J G Jr. Overview of the ACT program . Ninth DoT/NASA/FAA conference on fibrous composites in structural design-second NASA ACT Conference, FAA Report DoT/FAA/CT-92-25(II):577~599 [2] Holzwarth R C. An overview of the advanced lightweight aircraft fuselage structures (ALAFS) program . AIAA-96-1573-CP,1996 [3] Cox B N, Flanagan G. Handbook of analytical methods for textile composites . National Aeronautics and Space Administration Langley Research Center, Hampton, Virginia 23681-0001, NASA CR-4750, 1997 [4] Delbrey J. Database of mechanical properties of textile composites . National Aeronautics and Space Administration, Langley Research Center, Hampton, Virginia 23681-0001, NASA CR-4747, 1996 [5] Masters J E, Portanova M A. Standard test methods for textile composites . Lockheedmartin Engineering & Sciences Company, NASA CR-4751, 1996 [6] 任晓华. JSF制造技术综述[J]. 航空制造技术, 2002, (2):43~48 Ren Xiaohua. Summary of JSF manufacturing technology[J]. Aeronautical Manufacturing Technology, 2002, (2):43~48(in Chinese) [7] 桂良进. 缝合层合板基本力学性能和抗冲击性能研究 . 北京:北京航空航天大学飞行器设计与应用力学系, 2000 Gui Liangjin. Study on basal mechanical properties and impact resistance capabilities of stitched laminates . Beijing:Dept. of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, 2000(in Chinese) [8] 程小全. 复合材料层合板与蜂窝夹芯板低速冲击后压缩性能研究 . 北京:北京航空航天大学飞行器设计与应用力学系, 1998 Cheng Xiaoquan. Study on compressive properties of composite laminates and honeycomb core sandwich panels after low speed impact . Beijing:Dept. of Flight Vehicle Design and Applied Mechanics,Beijing University of Aeronautics and Astronautics, 1998(in Chinese) [9] Mouritz A P, Leong K H, Herszberg I. A review of the effect of stitched on the in-plane mechanical properties of fibre-reinforced polymer composites[J]. Composites-Part A, 1997, 28(12):979~991
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