HUANG Zhengming, ZHANG Ruojing. ON THE ULTIMATE STRENGTHOF A FIBER REINFORCED COMPOSITELAMINATE SUBJECTED TO LATERAL LOADS[J]. Acta Materiae Compositae Sinica, 2005, 22(2): 148-159.
Citation: HUANG Zhengming, ZHANG Ruojing. ON THE ULTIMATE STRENGTHOF A FIBER REINFORCED COMPOSITELAMINATE SUBJECTED TO LATERAL LOADS[J]. Acta Materiae Compositae Sinica, 2005, 22(2): 148-159.

ON THE ULTIMATE STRENGTHOF A FIBER REINFORCED COMPOSITELAMINATE SUBJECTED TO LATERAL LOADS

More Information
  • Received Date: April 14, 2004
  • Revised Date: June 20, 2004
  • It is well known that design and analysis for the ultimate load carrying capacity of a st ructure made of isot ropic materials can be accomplished only based on a st ress failure criterion (e. g. the first or the fourth st rengththeory int roduced in a mechanics of materials text book) . This is , however , not t rue for composites in general. It ispointed out in the paper that the ultimate failure of laminated composite beams subjected to bending cannot be figured out only based on a st ress failure criterion. Thus , the design and analysis for the ultimate load carrying capacityof composite st ructures require not only a st ress failure criterion but also a critical deformation related condition. Toshow this , some experimental evidences are summarized in the paper. Another purpose of this paper is to presentsome latest result s achieved by the authors in the relevant research areas especially in determination of the ultimatebending st rength of laminated composites. A number of challenging topics are also addressed in the paper.
  • Related Articles

    [1]YANG Xujing, ZHANG Liangsheng, LI Maojun, WANG Kaiyu, FANG Wenjun. Impregnation characteristics of carbon fiber composite during ultrasonic vibration assisted RTM process[J]. Acta Materiae Compositae Sinica, 2021, 38(12): 4161-4171. DOI: 10.13801/j.cnki.fhclxb.20210302.007
    [2]DUAN Jingbo, JIANG Tao, MA Hang, SHI Shengfeng, LU Ping. Influence of typical damages on composite wing vibration characteristics[J]. Acta Materiae Compositae Sinica, 2015, 32(2): 565-570. DOI: 10.13801/j.cnki.fhclxb.20140722.002
    [3]Vibration characteristics of 3D braided composites cantilever beam[J]. Acta Materiae Compositae Sinica, 2010, 27(6): 172-178.
    [4]ZHU Xiaopeng, LIANG Wei, MAI Hanchao. THREE-DIMENSIONAL SOLUTIONS FOR FREE VIBRATION OF THE MAGNETO-ELECTRIC-ELASTIC COMPOSITE LAMINATE[J]. Acta Materiae Compositae Sinica, 2005, 22(6): 130-134.
    [5]YANG Zi-chun. NONLINEAR THERMAL VIBRATION OF COMPOSITE LAMINATED PLATES ——PART Ⅱ: TEST[J]. Acta Materiae Compositae Sinica, 2000, 17(2): 119-122.
    [6]YANG Zi-chun. NONLINEAR THERMAL VIBRATION OF COMPOSITE LAMINATED PLATES ——PART Ⅰ: THEORY AND NUMERICAL ANALYSIS[J]. Acta Materiae Compositae Sinica, 2000, 17(2): 74-78.
    [7]WANG Jian-jiang, ZHAO Zhong-min, YE Min-hui, DU Xin-kang, WEN Jin-hua. INFLUENCES OF MECHANICAL VIBRATION ON MICROSTRUCTURE AND MECHANICAL PROPERTIES OF SHS CERAMIC-LINED PIPES[J]. Acta Materiae Compositae Sinica, 2000, 17(2): 55-59.
    [8]Xiang Chen, Chen Haoran, Guo Zhaopu. FLUID-STRUCTURE INTERACTION VIBRATION AND DYNAMIC RESPONSE OF COMPOSITE STIFFENED STRUCTURES[J]. Acta Materiae Compositae Sinica, 1996, 13(3): 100-104.
    [9]Deng Liangbo. VIBRATION OF LAMINATED PLATES CLAMPED AT FOUR EDGES RESTING ON WINKLER-PASTERNAK FOUNDATIONS[J]. Acta Materiae Compositae Sinica, 1993, 10(4): 49-56.
    [10]Chen Guibin, Zou Congqing. THE VIBRATION AND FLUTTER OF COMPOSITE MATERIAL LAMINATE[J]. Acta Materiae Compositae Sinica, 1992, 9(4): 1-6.

Catalog

    Article Metrics

    Article views (2029) PDF downloads (879) Cited by()
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return