FATIGUE CRACK-GROWTH RETARDATION INCONEL-600

被引：13

作者：

BROG, TK ^{[1
]}

JONES, JW ^{[1
]}

WAS, GS ^{[1
]}

机构：

[1] UNIV MICHIGAN,DEPT NUCL ENGN,ANN ARBOR,MI 48109

来源：

ENGINEERING FRACTURE MECHANICS | 1984年 / 20卷 / 02期

关键词：

Compendex;

D O I：

10.1016/0013-7944(84)90136-X

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：313 / 320

页数：8

共 19 条

[1]

[Anonymous], ASTM STP

[2]

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[3]

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DAVIDSON, DL ;

LANKFORD, J .

FATIGUE OF ENGINEERING MATERIALS AND STRUCTURES, 1979, 1 (04) :439-446

[5]

Elber W., 1970, Engineering Fracture Mechanics, V2, P37, DOI 10.1016/0013-7944(70)90028-7

[6]

Elber W, 1971, The Significance of Fatigue Crack Closure. Damage Tolerance in Aircraft Structures, P230, DOI DOI 10.1520/STP26680S

[7] FATIGUE CRACK CLOSURE AFTER OVERLOAD [J].

GAN, D ;

WEERTMAN, J .

ENGINEERING FRACTURE MECHANICS, 1983, 18 (01) :155-&

[8]

GAN D, 1981, ENG FRACTURE MECH, V15, P81

[9]

HARDRATH HF, 1961, NASATN0960

[10] DELAYED RETARDATION PHENOMENON OF FATIGUE CRACK GROWTH RESULTING FROM A SINGLE APPLICATION OF OVERLOAD [J].

MATSUOKA, S ;

TANAKA, K .

ENGINEERING FRACTURE MECHANICS, 1978, 10 (03) :515-525

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