FATIGUE CRACK-GROWTH UNDER RANDOM OVERLOADS SUPERIMPOSED ON CONSTANT-AMPLITUDE CYCLIC LOADING

被引:10
作者
ARONE, R
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D O I
10.1016/0013-7944(86)90053-6
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
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页码:223 / 232
页数:10
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共 30 条
[1]  
ADETIFA OA, 1976, ASTM STP, V595, P142
[2]  
Alzos W, 1976, ASTM STP, V595, P41
[3]  
[Anonymous], 1976, ASTM STP
[4]   MECHANISMS OF OVERLOAD EFFECT ON FATIGUE CRACK-PROPAGATION IN ALUMINUM-ALLOYS [J].
BATHIAS, C ;
VANCON, M .
ENGINEERING FRACTURE MECHANICS, 1978, 10 (02) :409-&
[5]  
Bernard P.J., 1976, ASTM STP, V595, P78
[6]   PREDICTION OF FATIGUE CRACK GROWTH UNDER FLIGHT-BY-FLIGHT LOADING [J].
BROEK, D ;
SMITH, SH .
ENGINEERING FRACTURE MECHANICS, 1979, 11 (01) :123-141
[7]   FATIGUE CRACK-GROWTH RETARDATION INCONEL-600 [J].
BROG, TK ;
JONES, JW ;
WAS, GS .
ENGINEERING FRACTURE MECHANICS, 1984, 20 (02) :313-320
[8]  
Buxbaum O., 1979, ASTM STP, V671, P5
[9]  
Cox D. R., 1962, RENEWAL THEORY
[10]  
de Koning A.U., 1981, ASTM STP, V743, P63