A THEORY FOR PROGRESSIVE MATRIX CRACKING IN COMPOSITE LAMINATES

被引：168

作者：

TAN, SC ^{[1
]}

NUISMER, RJ ^{[1
]}

机构：

[1] HERCULES INCORP,DEPT MAT TECHNOL,MAGNA,UT 84044

来源：

JOURNAL OF COMPOSITE MATERIALS | 1989年 / 23卷 / 10期

关键词：

D O I：

10.1177/002199838902301006

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

引用

页码：1029 / 1047

页数：19

共 16 条

[1]

CHOU PC, 1982, AFWALTR824083 AIR FO

[2] ANALYSIS OF PROGRESSIVE MATRIX CRACKING IN COMPOSITE LAMINATES .2. 1ST PLY FAILURE [J].

DVORAK, GJ ;

LAWS, N .

JOURNAL OF COMPOSITE MATERIALS, 1987, 21 (04) :309-329

[3] EXPERIMENTAL-DETERMINATION OF THE INSITU TRANSVERSE LAMINA STRENGTH IN GRAPHITE EPOXY LAMINATES [J].

FLAGGS, DL ;

KURAL, MH .

JOURNAL OF COMPOSITE MATERIALS, 1982, 16 (MAR) :103-116

[4] PREDICTION OF TENSILE MATRIX FAILURE IN COMPOSITE LAMINATES [J].

FLAGGS, DL .

JOURNAL OF COMPOSITE MATERIALS, 1985, 19 (01) :29-50

[5] MULTIPLE TRANSVERSE FRACTURE IN 90DEGREES CROSS-PLY LAMINATES OF A GLASS FIBER-REINFORCED POLYESTER [J].

GARRETT, KW ;

BAILEY, JE .

JOURNAL OF MATERIALS SCIENCE, 1977, 12 (01) :157-168

[6] BEHAVIOR OF COMPOSITE LAMINATES AFTER INITIAL FAILURES [J].

HAHN, HT ;

TSAI, SW .

JOURNAL OF COMPOSITE MATERIALS, 1974, 8 (JUL) :288-305

[7]

HAN YM, 1987, 2ND P AM SOC COMP TE, P503

[8]

HIGHSMITH AL, 1982, ASTM STP, V775, P103

[9]

KISTNER MD, 1985, ASTM STP, V864, P44

[10] CONSTITUTIVE RELATIONS OF A CRACKED COMPOSITE LAMINA [J].

NUISMER, RJ ;

TAN, SC .

JOURNAL OF COMPOSITE MATERIALS, 1988, 22 (04) :306-321

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