ON THE MECHANISMS AND BEHAVIOR OF OVERLOAD RETARDATION IN AISI-304 STAINLESS-STEEL

被引:109
作者
SHIN, CS
HSU, SH
机构
[1] Department of Mechanical Engineering, National Taiwan University, Taipei
关键词
TENSILE OVERLOAD; RETARDATION; CRACK CLOSURE; AISI-304 STAINLESS STEEL; R-RATIO EFFECT;
D O I
10.1016/0142-1123(93)90175-P
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The overload retardation phenomenon has been investigated in AISI 304 stainless steel under different baseline DELTAKs, overload ratios and R ratios. Both the crack growth and crack closure behaviour were carefully monitored. It was found that the extent and degree of retardation increase with overload ratio, decrease with R ratio, but are not correlated in a simple manner with the baseline DELTAK. For R less-than-or-equal-to 0.6, momentary acceleration followed by well-defined delayed retardation were observed. The crack growth behaviour before maximum retardation can be correctly predicted by Paris' law taking into account the experimentally measured crack closure value. Such a correlation failed beyond the maximum retardation point because of the occurrence of a discontinuous closure mechanism. Artificial introduction of crack closure by vacuum-infiltrating epoxy resin into the crack flanks also produced a similar retardation phenomenon. On the other hand, for R ratio greater-than-or-equal-to 0.65, immediate retardation was observed. Mechanisms that have been proposed to explain the overload retardation phenomenon are reviewed and examined against the current experimental observations. It is concluded that the major mechanism causing overload retardation is plasticity-induced crack closure. Secondary mechanisms, such as crack-tip blunting and residual compressive stress ahead of the crack tip, are significant only at high R ratios when crack closure is suppressed.
引用
收藏
页码:181 / 192
页数:12
相关论文
共 43 条
[1]   MECHANISMS OF OVERLOAD EFFECT ON FATIGUE CRACK-PROPAGATION IN ALUMINUM-ALLOYS [J].
BATHIAS, C ;
VANCON, M .
ENGINEERING FRACTURE MECHANICS, 1978, 10 (02) :409-&
[2]  
Bernard P.J., 1976, ASTM STP, V595, P78
[3]   OBSERVATION OF CRACK CLOSURE USING A CRACK MOUTH OPENING DISPLACEMENT GAUGE [J].
BRAHMA, KK ;
DASH, PK ;
DATTAGURU, B .
INTERNATIONAL JOURNAL OF FATIGUE, 1989, 11 (01) :37-41
[4]   EFFECTS OF TENSILE OVERLOADS ON CRACK CLOSURE AND CRACK-PROPAGATION RATES IN 7050 ALUMINUM [J].
BROWN, RD ;
WEERTMAN, J .
ENGINEERING FRACTURE MECHANICS, 1978, 10 (04) :867-878
[5]  
BUCCI RJ, 1980, ASTM STP, V714, P41
[6]   OBSERVATION OF CRACK-CLOSURE BEHAVIOR AFTER SINGLE OVERLOAD CYCLES IN 7075-T6 SINGLE-EDGE-NOTCHED SPECIMENS [J].
CHANANI, GR ;
MAYS, BJ .
ENGINEERING FRACTURE MECHANICS, 1977, 9 (01) :65-73
[7]  
Christensen RH., 1959, FATIGUE CRACKING FAT, P376
[8]   DECREASE IN CLOSURE AND DELAY OF FATIGUE CRACK-GROWTH IN PLANE-STRAIN [J].
DECASTRO, JTP ;
PARKS, DM .
SCRIPTA METALLURGICA, 1982, 16 (12) :1443-1446
[9]  
Elber W., 1970, Engineering Fracture Mechanics, V2, P37, DOI 10.1016/0013-7944(70)90028-7
[10]  
Elber W, 1971, SIGNIFICANCE FATIGUE