USE OF TIME-OF-FLIGHT C-SCANNING FOR ASSESSMENT OF IMPACT DAMAGE IN COMPOSITES

被引：22

作者：

PREUSS, TE ^{[1
]}

CLARK, G ^{[1
]}

机构：

[1] AERONAUT RES LABS,MELBOURNE,AUSTRALIA

来源：

COMPOSITES | 1988年 / 19卷 / 02期

关键词：

D O I：

10.1016/0010-4361(88)90725-2

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

引用

页码：145 / 148

页数：4

共 9 条

[1] BROUGHTON WR, 1986, NONDESTRUCTIVE TESTI, V23, P38
[2] DETECTION OF IMPACT DAMAGE IN CFRP LAMINATES
CANTWELL, WJ
MORTON, J
[J]. COMPOSITE STRUCTURES, 1985, 3 (3-4) : 241 - 257
[3] CLARK G, 1986, 422 AER RES LAB STRU
[4] HAGEMAIER DJ, 1979, MATER EVAL, P43
[5] POTTER RT, 1983, AGARD C CHARACTERISA
[6] PREUSS TE, 1987, ARLTM395 AIRCR MAT D
[7] Rosenfeld MS, 1981, FATIGUE FIBROUS COMP, P174
[8] SUBRAMANIAN K, 1987, ADV MATER P METAL PR, V2, P40
[9] THE QUALITY-CONTROL AND NON-DESTRUCTIVE EVALUATION OF COMPOSITE AEROSPACE COMPONENTS
TEAGLE, PR
[J]. COMPOSITES, 1983, 14 (02): : 115 - 128