2 CRITICAL STRESS INTENSITIES FOR THRESHOLD FATIGUE CRACK-PROPAGATION

被引：97
作者：
VASUDEVAN, AK
SADANANDA, K
LOUAT, N
机构：
[1] FAIRFAX MAT GRP,ALEXANDRIA,VA 22310
[2] USN,RES LAB,WASHINGTON,DC 20375
来源：
SCRIPTA METALLURGICA ET MATERIALIA | 1993年 / 28卷 / 01期
关键词：
D O I：
10.1016/0956-716X(93)90538-4
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
[No abstract available]
引用
收藏
页码：65 / 70
页数：6
相关论文
共 15 条
[1]   THRESHOLD RANGE AND OPENING STRESS INTENSITY FACTOR IN FATIGUE [J].
DOKER, H ;
MARCI, G .
INTERNATIONAL JOURNAL OF FATIGUE, 1983, 5 (04) :187-191
[2]  
DOKER H, 1984, 2ND INT C FAT THRESH, P275
[3]  
ELBER W, 1971, ASTM, P230
[4]  
GOODMAN J, 1930, MECHANICS APPLIED EN
[5]   HIGH-TEMPERATURE FAILURE OF AN ALUMINA SILICON-CARBIDE COMPOSITE UNDER CYCLIC LOADS - MECHANISMS OF FATIGUE CRACK-TIP DAMAGE [J].
HAN, LX ;
SURESH, S .
JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 1989, 72 (07) :1233-1238
[6]   SLOW FATIGUE CRACK GROWTH AND THRESHOLD BEHAVIOR IN AIR AND VACUUM OF COMMERCIAL ALUMINUM-ALLOYS [J].
KIRBY, BR ;
BEEVERS, CJ .
FATIGUE OF ENGINEERING MATERIALS AND STRUCTURES, 1979, 1 (02) :203-&
[7]   THE INFLUENCE OF AGE-HARDENING ON FATIGUE CRACK-PROPAGATION BEHAVIOR IN 7075 ALUMINUM-ALLOY IN VACUUM [J].
LAFARIEFRENOT, MC ;
GASC, C .
FATIGUE OF ENGINEERING MATERIALS AND STRUCTURES, 1983, 6 (04) :329-344
[8]  
Paris PC, 1961, TREND ENG, V13, P9, DOI DOI 10.11648/J.IJMEA.S.2015030201.11
[9]  
PETIT J, 1982, 4 P ECF FRACT, V2, P426
[10]  
SCHMIDT RA, 1973, ASTM STP536, P79
12