Modeling fatigue behavior of quasi-isotropic laminates

被引：0
|
作者：
Hesabi, Z. Razavi [2 ]
Kouchi, A. [3 ]
Beni, Y. Tadi [4 ]
Abadyan, M. [1 ]
机构：
[1] Islamic Azad Univ, Ramsar Branch, Engn Grp, Ramsar, Iran
[2] Sharif Univ Technol, Dept Mat Sci & Engn, Tehran, Iran
[3] Islamic Azad Univ, Naein Branch, Engn Grp, Naein, Iran
[4] Univ Shahrekord, Fac Engn, Shahrekord, Iran
来源：
11TH INTERNATIONAL CONFERENCE ON THE MECHANICAL BEHAVIOR OF MATERIALS (ICM11) | 2011年 / 10卷
关键词：
Quasi-isotropic Laminate; Fatigue Loading; Cyclic Loading;
D O I：
10.1016/j.proeng.2011.04.615
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
Fatigue behavior of quasi-isotropic carbon/epoxy laminates were studied, using six stacking sequences. Experimental results show that there is a significant stacking sequence effect on monotonic and cyclic performance of laminates. Though by changing the stacking sequence the difference between failure strength of the strongest and Weakest lay-ups reaches only to similar to 12 %, the difference between fatigue lives (cycles to failure) increased similar to 1000% in some loading regions. In addition, both linear and sigmoidal functions were examined to model the fatigue life behavior. (C) 2011 Published by Elsevier Ltd. Selection and/or peer-review under responsibility of ICM11
引用
收藏
页码：3764 / 3768
页数：5
相关论文
共 50 条
  • [21] SOME QUASI-ISOTROPIC LAMINATES ARE MORE ISOTROPIC THAN OTHERS
    Albazzan, Mazen A.
    Harik, Ramy
    Gurdal, Zafer
    Hartzell, Jesse
    IRF2018: PROCEEDINGS OF THE 6TH INTERNATIONAL CONFERENCE ON INTEGRITY-RELIABILITY-FAILURE, 2018, : 43 - 56
  • [22] Effect of cooling rate and stacking sequence on the fatigue behavior of notched quasi-isotropic AS4/PEEK laminates
    Vure, NRS
    Kriz, RD
    JOURNAL OF COMPOSITES TECHNOLOGY & RESEARCH, 1996, 18 (02): : 127 - 134
  • [23] LARGE DEFLECTION BEHAVIOR OF CIRCULAR QUASI-ISOTROPIC LAMINATES UNDER POINT LOADING
    KELKAR, A
    ELBER, W
    RAJU, IS
    AIAA JOURNAL, 1987, 25 (01) : 99 - 106
  • [24] Fatigue damage of quasi-isotropic composite laminates under tensile loading in different directions
    In-Kweon Kim
    Chang-Duk Kong
    Kyung-Seop Han
    KSME International Journal, 2000, 14 : 483 - 489
  • [25] Effects of toughened interlaminar layers on fatigue damage progress in quasi-isotropic CFRP laminates
    Ctr. for Collab. Research , Univ. Tokyo, 4-6-1 Komaba, M., Tokyo, Japan
    不详
    Int J Fatigue, 3 (235-242):
  • [26] Failure behavior of quasi-isotropic laminates with three-pin loaded holes
    Karakuzu, Ramazan
    Demirgoren, Ozgur
    Icten, Bulent Murat
    Deniz, Mehmet Emin
    MATERIALS & DESIGN, 2010, 31 (06) : 3029 - 3032
  • [27] Effects of toughened interlaminar layers on fatigue damage progress in quasi-isotropic CFRP laminates
    Takeda, N
    Kobayashi, S
    Ogihara, S
    Kobayashi, A
    INTERNATIONAL JOURNAL OF FATIGUE, 1999, 21 (03) : 235 - 242
  • [28] The influence of embedded optical fibres on the fatigue damage progress in quasi-isotropic CFRP laminates
    Surgeon, M
    Wevers, M
    JOURNAL OF COMPOSITE MATERIALS, 2001, 35 (11) : 931 - 940
  • [29] Fatigue damage of quasi-isotropic composite laminates under tensile loading in different directions
    Kim, IK
    Kong, CD
    Han, KS
    KSME INTERNATIONAL JOURNAL, 2000, 14 (05): : 483 - 489
  • [30] SPECIAL CLASS OF QUASI-ISOTROPIC LAMINATES FOR AEROSPACE APPLICATIONS
    Panda, Biranchi Narayan
    Bahubalendruni, M. V. A. Raju
    Biswal, B. B.
    M2D2015: PROCEEDINGS OF THE 6TH INTERNATIONAL CONFERENCE ON MECHANICS AND MATERIALS IN DESIGN, 2015, : 669 - 670
12345