TENSILE FRACTURE OF LAMINATES WITH CRACKS

[1] SENSITIVITY ANALYSIS OF THE DAMAGE ZONE MODEL [J]. COMPUTERS & STRUCTURES, 1986, 22 (04) : 669 - 676

[2] ARONSSON CG, 1984, OCT ASTM S COMP MAT

[3] ASTHON JE, 1970, THEORY LAMINATED PLA

[4] CRACK-TIP DAMAGE AND FRACTURE-TOUGHNESS OF BORON-ALUMINUM COMPOSITES [J]. JOURNAL OF COMPOSITE MATERIALS, 1979, 13 (APR) : 82 - 107

[5] FRACTURE-ANALYSIS OF NOTCHED COMPOSITES [J]. COMPUTERS & STRUCTURES, 1981, 13 (1-3) : 145 - 154

[6] STRESS INTENSITY AND CRACK OPENING OF COMPACT TENSION SPECIMENS [J]. ENGINEERING FRACTURE MECHANICS, 1979, 12 (01) : 99 - 101

[7] BACKLUND J, TENSILE FRACTURE L A

[8] Barenblatt GI., 1962, Adv Appl Mech, DOI [10.1016/s0065-2156(08)70121-2, DOI 10.1016/S0065-2156(08)70121-2]

[9] BROWN WF, 1970, ASTM STP, V463, P249

[10] CLARIN P, 1985, 855 ROYAL I TECHN DE

[1] SENSITIVITY ANALYSIS OF THE DAMAGE ZONE MODEL [J]. COMPUTERS & STRUCTURES, 1986, 22 (04) : 669 - 676

[2] ARONSSON CG, 1984, OCT ASTM S COMP MAT

[3] ASTHON JE, 1970, THEORY LAMINATED PLA

[4] CRACK-TIP DAMAGE AND FRACTURE-TOUGHNESS OF BORON-ALUMINUM COMPOSITES [J]. JOURNAL OF COMPOSITE MATERIALS, 1979, 13 (APR) : 82 - 107

[5] FRACTURE-ANALYSIS OF NOTCHED COMPOSITES [J]. COMPUTERS & STRUCTURES, 1981, 13 (1-3) : 145 - 154

[6] STRESS INTENSITY AND CRACK OPENING OF COMPACT TENSION SPECIMENS [J]. ENGINEERING FRACTURE MECHANICS, 1979, 12 (01) : 99 - 101

[7] BACKLUND J, TENSILE FRACTURE L A

[8] Barenblatt GI., 1962, Adv Appl Mech, DOI [10.1016/s0065-2156(08)70121-2, DOI 10.1016/S0065-2156(08)70121-2]

[9] BROWN WF, 1970, ASTM STP, V463, P249

[10] CLARIN P, 1985, 855 ROYAL I TECHN DE