ProfessorMariaCharalambides

Charalambides MN, Williams JG, 1995, Fracture Toughness characterisation of phenolic resin and its composite, Polymer Composites, Vol: 16, Pages: 17-28

• Cite

Charalambides MN, Williams JG, 1994, Mode I delamination of angle-ply/epoxy/Glass-fibre laminates exhibiting permanent deformation during fracture, Composites Science and Technology, Vol: 50, Pages: 187-196

• Cite

CHARALAMBIDES MN, WILLIAMS JG, 1994, MODE-I DELAMINATION OF ANGLE-PLY EPOXY-GLASS-FIBER LAMINATES EXHIBITING PERMANENT DEFORMATION DURING FRACTURE, COMPOSITES SCIENCE AND TECHNOLOGY, Vol: 50, Pages: 187-196, ISSN: 0266-3538

• Author Web Link
• Cite
• Citations: 10

Charalambides MN, Williams JG, 1993, Fracture toughness characterisation of phenolic resin and its composite, ASME Winter Annual Meeting, Use of Plastics and Plastic Composites: Materials and Mechanics Issues, Pages: 379-389

• Cite

Charalambides MN, Williams JG, 1993, Mode I delamination of angle-ply/epoxy/Glass-fibre laminates exhibiting permanent deformation during fracture, 2nd International Conference on Deformation and Fracture of Composites, Publisher: The Institute of Materials, Pages: 2-1-2-9

• Cite

CHARALAMBIDES M, KINLOCH AJ, WANG Y, WILLIAMS JGet al., 1992, ON THE ANALYSIS OF MIXED-MODE FAILURE, INTERNATIONAL JOURNAL OF FRACTURE, Vol: 54, Pages: 269-291, ISSN: 0376-9429

• Author Web Link
• Cite
• Citations: 139

Davies P, Kausch HH, Williams JG, Kinloch AJ, Charalambides MN, Pavan A, Moore DR, Prediger R, Robinson I, Burgoyne N, Friedrich K, Wittich H, Rebelo CA, Marques AT, Ramsteiner F, Melve B, Fischer M, Roux N, Martin D, Czarnocki P, Neville D, Verpoest I, Goffaux B, Lee R, Walls K, Trigwell N, Partridge IK, Jaussaud J, Andersen S, Giraud Y, Hale G, McGrath Get al., 1992, ROUND-ROBIN INTERLAMINAR FRACTURE TESTING OF CARBON-FIBER-REINFORCED EPOXY AND PEEK COMPOSITES, Composites Science and Technology, Vol: 43, Pages: 129-136, ISSN: 0266-3538

This paper summarizes results from a series of tests performed in eighteen laboratories with three specific aims: first, to establish the reproducibility of values from mode I and mode II tests carried out on two materials in different laboratories; secondly to investigate the differences between two data analyses; and finally to examine the influence of specimen thickness on mode I and mode II values. The materials tested, both unidirectional, were a relatively brittle carbon-fibre/epoxy laminate and a thermoplastic composite, carbon fibre/PEEK.

• Abstract
• Cite

DAVIES P, KAUSCH HH, WILLIAMS JG, KINLOCH AJ, CHARALAMBIDES MN, PAVAN A, MOORE DR, PREDIGER R, ROBINSON I, BURGOYNE N, FRIEDRICH K, WITTICH H, REBELO CA, MARQUES AT, RAMSTEINER F, MELVE B, FISCHER M, ROUX N, MARTIN D, CZARNOCKI P, NEVILLE D, VERPOEST I, GOFFAUX B, LEE R, WALLS K, TRIGWELL N, PARTRIDGE IK, JAUSSAUD J, ANDERSEN S, GIRAUD Y, HALE G, MCGRATH Get al., 1992, ROUND-ROBIN INTERLAMINAR FRACTURE TESTING OF CARBON-FIBER-REINFORCED EPOXY AND PEEK COMPOSITES, COMPOSITES SCIENCE AND TECHNOLOGY, Vol: 43, Pages: 129-136, ISSN: 0266-3538

• Author Web Link
• Cite
• Citations: 67