Numerical simulation of fatigue crack growth for curved cracks emanating from fastener holes in sheets by the MVCCI method

被引:1
|
作者
Theilig, H. [1 ]
Goth, M. [1 ]
Wuensche, M. [1 ]
机构
[1] Univ Appl Sci Zittau Gorlitz, Dept Mech Engn, Postfach 1455, D-02754 Zittau, Germany
来源
关键词
fastener hole; multiple crack systems; crack path simulation; curved increment; predictor-corrector procedure; improved modified virtual crack closure integral method; multiple mesh analysis;
D O I
10.4028/www.scientific.net/KEM.324-325.863
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The paper presents the results of a continued study of curved fatigue crack growth in a multiple arbitrarily pre-cracked isotropic sheet under plane stress loading. The predictor-corrector method (PCM) was extended in order to analyse the growth of multiple crack systems in a finite 2D structure. Together with the recently proposed improved mod fled virtual crack closure integral (MVCCI) method we can obtain accurate SIF values also for interacting cracks, and furthermore we can simulate fatigue crack growth of multiple crack systems in plane sheets under proportional mixed mode loading conditions. As a result, the program PCCS-2D is written to run within ANSYS to simulate interacting curved cracks. In order to check the accuracy and efficiency of the proposed method several example problems are solved. Especially curved cracks emanating from loaded fastener holes in sheets are analysed.
引用
收藏
页码:863 / +
页数:2
相关论文
共 50 条
  • [1] Numerical simulation of fatigue crack growth for corner cracks emanating from fastener holes
    Lin, XB
    Smith, RA
    NOTCH EFFECTS IN FATIGUE AND FRACTURE, 2001, 11 : 271 - 287
  • [2] Mixed mode fatigue growth of curved cracks emanating from fastener holes in aircraft lap joints
    J. H. Park
    S. N. Atluri
    Computational Mechanics, 1998, 21 : 477 - 482
  • [3] Mixed mode fatigue growth of curved cracks emanating from fastener holes in aircraft lap joints
    Park, JH
    Atluri, SN
    COMPUTATIONAL MECHANICS, 1998, 21 (06) : 477 - 482
  • [4] Fatigue crack growth prediction of small corner crack emanating from fastener holes in aircraft structures
    Kwon, JH
    Hwang, KJ
    Lee, SM
    Lee, JH
    KORUS 2003: 7TH KOREA-RUSSIA INTERNATIONAL SYMPOSIUM ON SCIENCE AND TECHNOLOGY, VOL 1 PROCEEDINGS: MACHINE PARTS AND MATERIALS PROCESSING, 2003, : 386 - 391
  • [5] The effect of transducer placement on the monitoring of fatigue cracks emanating from fastener holes
    Cobb, A. C.
    Michaels, J. E.
    Michaels, T. E.
    REVIEW OF PROGRESS IN QUANTITATIVE NONDESTRUCTIVE EVALUATION, VOLS 26A AND 26B, 2007, 894 : 1516 - +
  • [6] STATISTICS OF FATIGUE CRACK GROWTH IN FASTENER HOLES
    Harlow, D. Gary
    16TH ISSAT INTERNATIONAL CONFERENCE ON RELIABILITY AND QUALITY IN DESIGN, 2010, : 130 - 134
  • [7] Analysis of curved cracks emanating from adjacent holes
    Wang, XD
    Meguid, SA
    Papanikos, P
    ENGINEERING FRACTURE MECHANICS, 1999, 64 (03) : 337 - 355
  • [8] Fracture and fatigue analysis of curved or kinked cracks near fastener holes
    Chow, WT
    Atluri, SN
    FINITE ELEMENTS IN ANALYSIS AND DESIGN, 1996, 23 (2-4) : 91 - 100
  • [9] Experimental and analytical analyses of fatigue crack growth in sheets with multiple holes and cracks
    Li Z.
    Xu W.
    Zhang X.
    Yu Y.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2018, 39 (07):
  • [10] EFFECT OF CRACK CLOSURE ON ULTRASONIC DETECTION OF FATIGUE CRACKS AT FASTENER HOLES
    Bowles, S. J.
    Harding, C. A.
    Hugo, G. R.
    REVIEW OF PROGRESS IN QUANTITATIVE NONDESTRUCTIVE EVALUATION, VOLS 28A AND 28B, 2009, 1096 : 1878 - 1885