FATIGUE CRACK-PROPAGATION IN 2090 ALUMINUM-LITHIUM ALLOY - EFFECT OF COMPRESSION OVERLOAD CYCLES

被引:23
作者
YU, W
RITCHIE, RO
机构
[1] Univ of California, Berkeley, CA,, USA, Univ of California, Berkeley, CA, USA
来源
JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME | 1987年 / 109卷 / 01期
关键词
D O I
10.1115/1.3225939
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
31
引用
收藏
页码:81 / 85
页数:5
相关论文
共 30 条
[1]  
AU P, 1983, AGARD C P, V328
[2]  
BAKER C, 1986, 3RD P INT AL LI C OX
[3]  
BRETZ PE, 1986, ALUMINIUM LITHIUM AL, V3, P47
[4]   THE EFFECT OF MICROSTRUCTURE AND ENVIRONMENT ON FATIGUE CRACK CLOSURE OF 7475-ALUMINUM ALLOY [J].
CARTER, RD ;
LEE, EW ;
STARKE, EA ;
BEEVERS, CJ .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1984, 15 (03) :555-563
[5]  
COYNE EJ, 1981, ALUMINUM LITHIUM ALL, P293
[6]   CHARACTERISTICS OF STAGE I FATIGUE FRACTURE IN A HIGH-STRENGTH NICKEL ALLOY [J].
GELL, M ;
LEVERANT, GR .
ACTA METALLURGICA, 1968, 16 (04) :553-&
[7]  
Glazer J., 1986, ADV CRYOGEN ENG, V32, P397
[8]  
Harris S., 1984, ALUM LITHIUM ALLOYS, VII, P219
[9]  
JATA KV, 1986, ALUMINIUM LITHIUM AL, V3, P247
[10]   THE EFFECT OF COPPER CONTENT AND DEGREE OF RECRYSTALLIZATION ON THE FATIGUE RESISTANCE OF 7XXX-TYPE ALUMINUM-ALLOYS .2. FATIGUE CRACK-PROPAGATION [J].
LIN, FS ;
STARKE, EA .
MATERIALS SCIENCE AND ENGINEERING, 1980, 43 (01) :65-76