2007 ICCM-16 Kyoto Japan
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ICCM-16 Sixteenth International Conference on Composite Materials

July/11 (Wed.) -- Room I

July -- 8(Sun.) / 9(Mon.) / 10(Tue.) / 11(Wed.) / 12(Thr.) / 13(Fri.)

July/11(Wed.) -- Room A / B-2 / F / G / H / I / J / K / Poster Session (B-1)

Wednesday Morning (July 11) -- Room I: 9:20-13:20
Session Title: Mechanics of Matrix Crack and other Damage
Presenters Name Affiliation Country Paper Title pdf
Chairperson(s): Satoshi Kobayashi
Jian Yang University of Birmingham UK A LAYER-WISE FOURIER EXPANSION APPROACH FOR STRESS TRANSFER IN CROSS-PLY LAMINATES WITH TRANSVERSE MATRIX CRACKS WeIM1-01
Jianqiao Ye University of Leeds UK
Abdul-Salam Kaddour Qinetiq UK MULTI-AXIAL NOTCHED STRENGTH ENVELOPES FOR AEROSPACE COMPOSITE LAMINATES WeIM1-02
Shuguang Li University of Manchester UK Reduction of transverse shear stiffnesses of transversely cracked laminates WeIM1-03
Farrukh Hafeez University of Manchester UK
W Steven Johnson Georgia Institute of Technology USA Ply Modifications to Alter Damage Initiation and Progression In Laminates Containing Holes WeIM1-04
Paul J Treasurer Georgia Institute of Technology US
Hamid Razi Boeing Commercial Aircraft US
Daniel Hoffman Boeing Commercial Aircraft US
Session Title: Benchmarking of failure criteria under 3D loading: (WWFE-II, Specialist Session)
Organizers Abdul-Salam Kaddour Qinetiq UK
Mike Hinton Qinetiq UK
Chairperson(s):
Abdul-Salam Kaddour Qinetiq UK THE SECOND WORLD-WIDE FAILURE EXERCISE: BENCHMARKING OF FAILURE CRITERIA UNDER TRIAXIAL STRESSES FOR FIBRE-REINFORCED POLYMER COMPOSITES WeIM1-05
Mike Hinton Qinetiq UK
Danny J.L. Van Hemelrijck Vrije Universiteit Brussel Belgium Biaxial testing of fibre reinforced composites WeIM1-06
Carla Ramault Vrije Universiteit Brussel Belgium
Andreas Makris Vrije Universiteit Brussel Belgium
Andrew Clarke Qinetiq UK
C. Williamson Qinetiq UK
Jeffry S Welsh Air Force Research Laboratory USA EXPERIMENTAL AND NUMERICAL FAILURE PREDICTIONS OF BIAXIALLY-LOADED QUASI-ISOTROPIC CARBON COMPOSITES WeIM1-07
J. Steve Mayes Air Force Research Laboratory USA
Adam C Biskner Air Force Research Laboratory USA
Jens H. Andreasen Aalborg University Denmark Interface to Interface Core Cracks in Sandwich Structures WeIM1-08
Johnny Jakobsen Aalborg University Denmark
Anders Lyckegaard NKT Flexibles I/S, Brondby, Denmark Denmark
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Wednesday Afternoon (July 11) -- Room I: 13:20-(18:00)
Session Title: Benchmarking of damage and continuum mechanics failure criteria: (WWFE-III, Specialist Session)
Name Affiliation Country Paper Title pdf
Organizers Abdul-Salam Kaddour Qinetiq UK
Mike Hinton Qinetiq UK
Chairperson(s)
Abdul-Salam Kaddour Qinetiq UK DAMAGE THEORIES FOR FIBRE-REINFORCED POLYMER COMPOSITES: THE THIRD WORLD-WIDE FAILURE EXERCISE (WWFE-III) WeIA1-01
Mike Hinton Qinetiq UK
S Li University of Manchester UK
P A Smith University of Surrey UK
L Neil McCartney National Physical Laboratory UK Models to predict ply cracking and its effects on laminate properties WeIA1-02
Ramesh Talreja Texas A&M University USA CONTINUUM DAMAGE MECHANICS: A MODELING APPROACH FOR COMPREHENSIVE ASSESSMENT OF SUBCRITICAL DAMAGE IN COMPOSITES WeIA1-03
Chandra Veer Singh Texas A&M University US
Atsushi Hosoi Waseda University Japan Interaction between transverse cracks and edge delamination considering free-edge effects in composite laminates WeIA1-04
Shinako Yagi Waseda University Japan
Hiroyuki Kawada Waseda University Japan
Keiichi Nagata Toray Industries, Inc. Japan
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