Three-dimensional stress intensity factor calibration for a stiffened cracked plate

被引:15
作者
Moreira, P. M. G. P. [1 ]
Pastrama, S. D. [2 ]
de Castro, P. M. S. T. [3 ]
机构
[1] INEGI Inst Mech Engn & Ind Management, Oporto, Portugal
[2] Univ Politehn Bucuresti, Dept Strength Mat, Bucharest, Romania
[3] Univ Porto, Dept Mech Engn, Oporto, Portugal
关键词
Stress intensity factor; Stiffened panel; J-Integral; Plane stain behaviour; Opening stress; PANELS; PROPAGATION;
D O I
10.1016/j.engfracmech.2009.07.003
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Three-dimensional finite element analyses are used in this paper to calibrate the stress intensity factor in a cracked stiffened plate subjected to remote uniform traction. An accurate numerical determination of the stress field and stress intensity variation through the thickness of a central cracked plate was first carried out in order to evaluate three-dimensional effects. A stiffened cracked plate was then analysed, taking into account the results and the conclusions obtained in the previous study. Such a structure was chosen due to the growing interest for large integral metallic structures for aircraft applications, following the continuous need for low cost and the emergence of new technologies. The J-Integral technique was used to calculate the values of the stress intensity factor along the plate thickness. The plane strain behaviour near the crack front and the variation of the opening stress are discussed. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2298 / 2308
页数:11
相关论文
共 28 条
[11]  
MOREIRA PMG, 2008, THESIS U PORTO PORTO
[12]   The computational post-buckling analysis of fuselage stiffened panels loaded in shear [J].
Murphy, A ;
Price, M ;
Lynch, C ;
Gibson, A .
THIN-WALLED STRUCTURES, 2005, 43 (09) :1455-1474
[13]   3-DIMENSIONAL STRESS-FIELD NEAR THE CRACK FRONT OF A THIN ELASTIC PLATE [J].
NAKAMURA, T ;
PARKS, DM .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1988, 55 (04) :805-813
[14]  
Paris PC, 1961, Trends Engineering, V13, P9
[15]  
PASTRAMA S, 2006, 10 PORT C FRACT GUIM
[16]  
RAJU I, 1977, TND8414 NASA CTR AER
[17]   INFLUENCE OF BIAXIAL LOADING ON ANALYSIS OF CRACKED STIFFENED PANELS [J].
RATWANI, MM ;
WILHEM, DP .
ENGINEERING FRACTURE MECHANICS, 1979, 11 (03) :585-593
[18]  
Rice J. R., 1968, FRACTURE, V2, P191
[19]  
Rooke D P., 1977, Fracture Mechanics in Engineering Practice
[20]  
Rooke D.P., 1976, COMPENDIUM STRESS IN