RELATIONSHIP BETWEEN FATIGUE LIFE DISTRIBUTION, NOTCH CONFIGURATION, AND S-N CURVE OF A 2024-T4 ALUMINUM-ALLOY

被引:27
作者
SHIMOKAWA, T
HAMAGUCHI, Y
机构
来源
JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME | 1985年 / 107卷 / 03期
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D O I
10.1115/1.3225804
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
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页码:214 / 220
页数:7
相关论文
共 12 条
[1]  
BASTENAIRE FA, 1963, FATIGUE AIRCRAFT STR, P53
[2]  
BASTENAIRE FA, 1972, ASTM STP, V511, P3
[3]  
DUNSBY JA, 1969, MATER RES STANDARD, V9, P15
[4]  
LIU HW, 1960, NASA TN D647
[5]  
MANN JY, 1981, P FATIGUE 81, P390
[6]  
MATOLCSY M., 1969, MATERIALPRUFUNG, V11, P196
[7]  
MURAKAMI Y, 1979, T JAPAN SOC MECH ENG, V45, P998
[8]  
SHIMOKAWA T, 1979, T JPN SOC AERONAUT S, V21, P225
[9]  
SHIMOKAWA T, 1977, NAL TR412T
[10]  
Sinclair GM, 1953, T AM SOC MECH ENG, V75, P867