Modeling fatigue crack growth in a bimaterial specimen with the configurational forces concept

被引:29
|
作者
Kolednik, Otmar [1 ]
Predan, Jozef [2 ]
Gubeljak, Nenad [2 ]
Fischer, Dieter F. [3 ]
机构
[1] Austrian Acad Sci, Erich Schmid Inst Mat Sci, A-8700 Leoben, Austria
[2] Univ Maribor, Fac Mech Engn, SI-2000 Maribor, Slovenia
[3] Univ Leoben, Inst Mech, A-8700 Leoben, Austria
关键词
Configurational forces; Fatigue crack growth; Inhomogeneous material; Crack-tip shielding; Finite element modeling; ELASTIC-PLASTIC MATERIALS; INHOMOGENEOUS MATERIALS; DRIVING-FORCE; FRACTURE-BEHAVIOR; YIELD STRESSES; INTERFACE; PROPAGATION; THRESHOLD; COMPOSITE; SYSTEM;
D O I
10.1016/j.msea.2009.04.059
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
A two-dimensional finite element analysis is performed to model the behavior of fatigue cracks in bimaterial specimens made of diffusion-bonded ARMCO-iron and SAE 4340 steel with an interface perpendicular to the crack plane. The numerical analyses are based on experiments conducted by Pippan et al. [Mater. Sci. Eng. A 283 (2000) 225-233]. The concept of configurational forces is used to evaluate by post-processing the crack-tip shielding and anti-shielding effects that occur due to the differences in yield stress, hardening and coefficients of thermal expansion of ARMCO-iron and SAE 4340 steel. For given values of applied stress intensity range Delta K(app) and applied load ratio R(app), the near-tip J-integral J(tip) is calculated at the maximum and minimum load. To allow for crack closure, the effective near-tip stress intensity range Delta K(eff.tip) is evaluated from the near-tip stress intensity range Delta K(tip) and the near-tip load ratio R(tip). Calibration curves for homogeneous ARMCO-iron and SAE 4340 steel are used to calculate the crack growth rate da/dN from the values of Delta K(eff.tip). The distance between interface and crack tip L is varied to simulate the behavior of a growing crack. The computed curves da/dN versus L curves are in good agreement with the experimental results. (C) 2009 Elsevier B.V. All rights reserved.
引用
收藏
页码:172 / 183
页数:12
相关论文
共 50 条
  • [21] MODE II FATIGUE CRACK GROWTH SPECIMEN DEVELOPMENT.
    Buzzard, Robert J.
    Gross, Bernard
    Srawley, John E.
    NASA Technical Memorandum, 1984,
  • [22] EFFECT OF SPECIMEN THICKNESS ON FATIGUE CRACK GROWTH-RATE
    SULLIVAN, AM
    CROOKER, TW
    REPORT OF NRL PROGRESS, 1975, (JUL): : 7 - 9
  • [23] INFLUENCE OF SPECIMEN GEOMETRY ON MODE OF FATIGUE CRACK GROWTH IN ALUMINIUM
    PLUMBRIDGE, WJ
    RYDER, DA
    ACTA METALLURGICA, 1969, 17 (12): : 1449 - +
  • [24] Influence of test specimen thickness on the fatigue crack growth of rubber
    Stocek, R.
    Kipscholl, R.
    CONSTITUTIVE MODELS FOR RUBBER X, 2017, : 347 - 350
  • [25] Influence of specimen geometry on the random load fatigue crack growth
    Radon, JC
    Nikbin, K
    FATIGUE AND FRACTURE MECHANICS: 32ND VOLUME, 2002, 1406 : 88 - 104
  • [26] FATIGUE CRACK GROWTH SPECIMEN CONFIGURATION WITH COMPRESSIVE LOADS PRESENT
    STEPHENS, RI
    INTERNATIONAL JOURNAL OF FRACTURE, 1976, 12 (02) : 323 - 326
  • [27] Influence of specimen geometry on the random load fatigue crack growth
    Radon, J.C.
    Nikbin, K.
    ASTM Special Technical Publication, 2001, (1406): : 88 - 104
  • [28] MINIATURIZED FATIGUE CRACK-GROWTH SPECIMEN TECHNOLOGY AND RESULTS
    PUIGH, RJ
    BAUER, RE
    ERMI, AM
    CHIN, BA
    JOURNAL OF NUCLEAR MATERIALS, 1982, 103 (1-3) : 1501 - 1504
  • [29] Characterization of fatigue crack growth by cyclic material forces
    Khodor, Jad
    Ozenc, Kaan
    Lin, Guoyu
    Kaliske, Michael
    ENGINEERING FRACTURE MECHANICS, 2021, 243
  • [30] Characterization of fatigue crack growth by cyclic material forces
    Khodor, Jad
    Ozenc, Kaan
    Lin, Guoyu
    Kaliske, Michael
    ENGINEERING FRACTURE MECHANICS, 2021, 243