The stress intensity factor for a cracked stiffened sheet repaired with an adhesively bonded composite patch

被引：0
|
作者：
C. N. Duong
J. Yu
机构：
[1] McDonnell Douglas Aerospace,
来源：
International Journal of Fracture | 1997年 / 84卷
关键词：
Stress intensity factor; adhesively bonded composite patch; cracked stiffened sheet.;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The problem of a cracked, stiffened metallic sheet adhesively bonded by a composite patch is analyzed. The composite patch is assumed to be either an infinite orthotropic sheet or an infinite orthotropic strip normal to the crack. Due to the high stress concentration around the crack and on the interface, an elliptical disbond is assumed to exist around the crack. The crack is asymmetric with respect to the stiffener's locations as well as to the patch's center. The effect of thermal stresses in curing process is also considered. The fracture problem is solved by the displacement compatibility method, using the complex variable approach and the Fourier integral transform method.
引用
收藏
页码：37 / 60
页数：23
相关论文
共 50 条
  • [1] The stress intensity factor for a cracked stiffened sheet repaired with an adhesively bonded composite patch
    Duong, CN
    Yu, J
    [J]. INTERNATIONAL JOURNAL OF FRACTURE, 1997, 84 (01) : 37 - 60
  • [2] Stress Analysis of Cracked Metallic Aircraft Structure Adhesively Repaired with Composite Patch
    Su, Weiguo
    Zou, Lan
    Mu, Zhitao
    Li, Xudong
    [J]. PROCEEDINGS OF THE FIRST SYMPOSIUM ON AVIATION MAINTENANCE AND MANAGEMENT-VOL II, 2014, 297 : 369 - 377
  • [3] Fatigue crack growth analysis of stiffened cracked panel repaired with bonded composite patch
    Sabelkin, V.
    Mall, S.
    Avram, J. B.
    [J]. ENGINEERING FRACTURE MECHANICS, 2006, 73 (11) : 1553 - 1567
  • [4] EFFECT OF BONDED COMPOSITE PATCH ON THE STRESS INTENSITY FACTOR FOR A CENTER-CRACKED PLATE
    Aabid, Abdul
    Hrairi, Meftah
    Ali, Jaffar Syed Mohamed
    Abuzaid, Ahmed
    [J]. IIUM ENGINEERING JOURNAL, 2019, 20 (02): : 211 - 221
  • [5] Analysis of the disbond effect on the stress intensity factor variation for repaired cracks with bonded composite patch
    Amiri, A.
    Bouiadjra, B. Bachir
    Serier, B.
    Belhouari, M.
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART L-JOURNAL OF MATERIALS-DESIGN AND APPLICATIONS, 2006, 220 (L2) : 91 - 93
  • [6] STRESS INTENSITY FACTORS FOR A CRACKED STIFFENED SHEET WITH CRACKED STIFFENERS
    NISHIMURA, T
    [J]. JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 1991, 113 (01): : 119 - 124
  • [7] Progressive edge cracked aluminium plate repaired with adhesively bonded composite patch under full width disbond
    Ouinas, D.
    Bouiadjra, B. Bachir
    Himouri, S.
    Benderdouche, N.
    [J]. COMPOSITES PART B-ENGINEERING, 2012, 43 (02) : 805 - 811
  • [8] Investigation into cracked aluminum plate repaired with bonded composite patch
    Sabelkin, V.
    Mall, S.
    Hansen, M. A.
    Vandawaker, R. M.
    Derriso, M.
    [J]. COMPOSITE STRUCTURES, 2007, 79 (01) : 55 - 66
  • [9] Initiation and progression of composite patch debonding in adhesively repaired cracked metallic sheets
    Papanikos, P.
    Tserpes, K. I.
    Pantelakis, Sp.
    [J]. COMPOSITE STRUCTURES, 2007, 81 (02) : 303 - 311
  • [10] Stress intensity factor for repaired crack with bonded composite patch under thermo-mechanical loading
    Mhamdia, R.
    Bouadjra, B. Bachir
    Serier, B.
    Ouddad, W.
    Feaugas, X.
    Touzain, S.
    [J]. JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2011, 30 (05) : 416 - 424
12345