《cyclicloadingofacrackedsheetapproachesandresults:循环载荷的裂纹板的方法和结果》由会员分享,可在线阅读,更多相关《cyclicloadingofacrackedsheetapproachesandresults:循环载荷的裂纹板的方法和结果(10页珍藏版)》请在金锄头文库上搜索。
1、The asymptotic study of fatigue crack growth based on continuum damage mechanics,Zhao J., Zhang X. The asymptotic study of fatigue crack growth based on damage mechanics/ Engn. Fracture Mechanics. 1995. V. 50. 1. P. 131-141. Li J., Recho N. Methodes asymptotiques en mecanique de la rupture. Paris: H
2、ermes Science Publications, 2002. 262 p. Astafiev V.I., Radayev Y.N., Stepanova L.V. Nonlinear fracture mechanics. Samara: Samara State University, 2001. 632 p. Stepanova L.V. Mathematical methods of fracture mechanics. Moscow: Fizmatlit, 2009. 336 p. Astafjev V.I., Grigorova T.V., Pastuchov V.A. In
3、fluence of continuum damage on stress distribution near a tip of a growing crack under creep conditions/ procedings of the International Colloquium Mechanics of creep brittle materials 2, University of Leicester, UK, 1991. P. 49-61.,The asymptotic study of fatigue crack growth based on continuum dam
4、age mechanics,Consider a fatigue growing crack lying on the x-axis with the coordinate origin located at the moving crack tip,The asymptotic study of fatigue crack growth based on continuum damage mechanics,The essence of continuum damage mechanics is characterized by material deterioration coupled
5、constitutive equations. Under the assumption of linear elasticity a stiffness reduction based stress-strain relationship is applied as The kinetic law of damage evolution The equilibrium equations,The asymptotic study of fatigue crack growth based on continuum damage mechanics,The compatibility equa
6、tion The constitutive equations The constitutive equations for plane stress conditions The constitutive equations for plane strain conditions,The asymptotic study of fatigue crack growth based on continuum damage mechanics,The traditional traction free conditions on crack surfaces The Airy stress fu
7、nction The Airy stress function can be presented in the form The Mode I stress field components at the crack tip behave as follows,The asymptotic study of fatigue crack growth based on continuum damage mechanics,The damage field around the crack tip can be presented as The strain components are give
8、n as From the compatibility equation one can obtain (for plane stress) one can obtain (for plane strain),The asymptotic study of fatigue crack growth based on continuum damage mechanics,The damage evolution law allows to obtain The symmetry of the stress and damage fields around the crack tip The no
9、rmalizing condition is chosen as The regularity requirement The traction free conditions,The asymptotic study of fatigue crack growth based on continuum damage mechanics,The totally damaged zone needs to be modeled in the vicinity of the crack tip The analytical result The stress and damage fields a
10、round the crack tip,The asymptotic study of fatigue crack growth based on continuum damage mechanics,The asymptotic study of fatigue crack growth based on continuum damage mechanics,The analytical presentation of stress, strain and continuity fields both for plane strain and plane stress conditions
11、is given. The results obtained differ from Zhao and Zhangs solution where the original formulation of the problem for plane stress conditions has been proposed. An analytical solution of the nonlinear eigenvalue problem arising from the fatigue crack growth problem in a damaged medium in coupled formulation is obtained. The perturbation technique is used. The method allows to find the analytical formula expressing the eigenvalue as the function of parameters of the damage evolution law.,