MODELING OF IMPACT DAMAGE IN COMPOSITE LAMINATES

[11] USE OF TIME-OF-FLIGHT C-SCANNING FOR ASSESSMENT OF IMPACT DAMAGE IN COMPOSITES [J]. COMPOSITES, 1988, 19 (02): : 145 - 148

[12] PREUSS TE, 1987, DSTO395 AER RES LAB

[13] MATRIX FRACTOGRAPHY OF FIBER-REINFORCED EPOXY COMPOSITES [J]. COMPOSITES, 1986, 17 (04): : 289 - 303

[14] ROSENFELD MS, 1981, ASTM STP723

[15] EFFECT OF LOAD DURATION ON THE FATIGUE BEHAVIOR OF GRAPHITE EPOXY LAMINATES CONTAINING DELAMINATIONS [J]. COMPOSITES, 1988, 19 (03): : 217 - 228

[16] Wang ASD, 1980, J COMPOS MATER, V14, P71, DOI 10.1177/002199838001400106.

[17] WANG SS, 1982, 4 P INT C COMP MAT, V1, P287

[11] USE OF TIME-OF-FLIGHT C-SCANNING FOR ASSESSMENT OF IMPACT DAMAGE IN COMPOSITES [J]. COMPOSITES, 1988, 19 (02): : 145 - 148

[12] PREUSS TE, 1987, DSTO395 AER RES LAB

[13] MATRIX FRACTOGRAPHY OF FIBER-REINFORCED EPOXY COMPOSITES [J]. COMPOSITES, 1986, 17 (04): : 289 - 303

[14] ROSENFELD MS, 1981, ASTM STP723

[15] EFFECT OF LOAD DURATION ON THE FATIGUE BEHAVIOR OF GRAPHITE EPOXY LAMINATES CONTAINING DELAMINATIONS [J]. COMPOSITES, 1988, 19 (03): : 217 - 228

[16] Wang ASD, 1980, J COMPOS MATER, V14, P71, DOI 10.1177/002199838001400106.

[17] WANG SS, 1982, 4 P INT C COMP MAT, V1, P287