IMPACT AND SUBSEQUENT FATIGUE DAMAGE GROWTH IN CARBON-FIBER LAMINATES

被引：44

作者：

CANTWELL, WJ ^{[1
]}

CURTIS, PT ^{[1
]}

MORTON, J ^{[1
]}

机构：

[1] ROYAL AIRCRAFT ESTAB,DEPT MAT & STRUCT,FARNBOROUGH GU14 6TD,HANTS,ENGLAND

来源：

关键词：

D O I：

10.1016/0142-1123(84)90022-7

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

页码：113 / 118

页数：6

共 15 条

[1]

ADAMS DF, ASTM STP AM SOC TEST, V617, P409

[2]

BEAUMONT PWR, 1974, ASTM STP, V568, P134

BISHOP, SM .

COMPOSITES, 1983, 14 (03) :201-205

[4]

BISHOP SM, 1983, RAE TR83010 ROYAL AI

[5]

BISHOP SM, 1983, Patent No. 6653

[6]

BRADSHAW FJ, 1973, RAE TR72240 ROYAL AI

[7]

CARD MF, 1980, AGARD CP, V288

[8]

CHAMIS CC, 1971, NASA TND6463

[9]

DOREY G, FRACTURE COMPOSITES

[10]

DOREY G, 1977, AHS NASA AMES C