INTERLAMINAR FRACTURE-TOUGHNESS TESTING OF COMPOSITE MODE-I AND MODE-II DCB SPECIMENS

被引:22
作者
ILCEWICZ, LB
KEARY, PE
TROSTLE, J
机构
[1] Boeing Commercial Airplane Co,, Seattle, WA, USA, Boeing Commercial Airplane Co, Seattle, WA, USA
关键词
D O I
10.1002/pen.760280908
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
57
引用
收藏
页码:592 / 604
页数:13
相关论文
共 57 条
  • [1] ASHIZAWA M, 1983, 6TH DOD NASA C FIBR
  • [2] BASCOM WD, 1980, COMPOSITES, V2, P9
  • [3] BASCOM WD, 1984, 29TH NAT SAMPE S, P970
  • [4] Begley J. A., 1972, ASTM STP, V514, P1
  • [5] BENZEGGAGH ML, 1985, 5TH INT C COMP MAT, P127
  • [6] BRADLEY WL, 1986, JUN P INT S COMP MAT, P445
  • [7] BRADLEY WL, 1985, ASTM STP, V876, P389
  • [8] BRADLEY WL, 1982, AFOSRTR831018
  • [9] THE CHARACTERIZATION OF MODE-I DELAMINATION FAILURE IN NON-WOVEN, MULTIDIRECTIONAL LAMINATES
    CHAI, H
    [J]. COMPOSITES, 1984, 15 (04): : 277 - 290
  • [10] CORLETO C, 1986, APR ASTM D300202 TAS