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

July/12 (Thr.) -- Room B-2

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

July/12(Thr.) -- Room A / B-2 / F / G / H / I / J / K

Thursday Morning (July 12) -- Room B-2: 9:20-14:20
Session Title: Delamination : Characterization I (Specialist Session)
Name Affiliation Country Paper Title pdf
Organizers T Kevin O'Brien U.S. Army Research Laboratory USA
Paul Robinson Imperial College London UK
Masaki Hojo Kyoto University Japan
Chairperson(s):
Keynote Emile S Greenhalgh Imperial College London UK Fractographic observations on delamination growth mechanisms ThBM1-01
Paul Robinson Imperial College London UK
Charlotte Rogers Imperial College London UK
Paul Robinson Imperial College London UK INTERFACE EFFECTS IN MODE II INTERLAMINAR TOUGHNESS TESTING OF UNIDIRECTIONAL COMPOSITES ThBM1-02
Stephen Message Imperial College London UK
Adrian F. Gill Imperial College London UK Effect of RTM defects on Mode I & II delamination behaviour of 5HS woven composites ThBM1-03
Paul Robinson Imperial College London UK
Dennis Hitchings Imperial College London UK
Silvestre Pinho Imperial College London UK
John Sargent Imperial College London UK
Shinji Ogihara Tokyo University of Science Japan Mode III Interlaminar Fracture Toughness in Laminated Composites ThBM1-04
Katsuhiro Matsuda Tokyo University of Science Japan
Session Title: Delamination : Characterization II (Specialist Session)
Chairperson(s):
Takayuki Kusaka Ritsumeikan University Japan Mode I Fracture Behavior and Toughening Mechanism of Zanchor Reinforced Composites ThBM1-05
Yuhei Yamaguchi Ritsumeikan University Japan
Keiko Watanabe Ritsumeikan University Japan
Masaki Hojo Kyoto University Japan
Toshiyasu Fukuoka Mitsubishi Heavy Industries Japan
Keiko Watanabe Ritsumeikan University Japan Mode II Fracture Behavior and Toughening Mechanism of Zanchor Reinforced Composites ThBM1-06
Takayuki Kusaka Ritsumeikan University Japan
Masaki Hojo Kyoto University Japan
Toshiyasu Fukuoka Mitsubishi Heavy Industries, Ltd. Japan
Masayasu Ishibashi Shikibo, Ltd. Japan
Kozue Nakane Tokyo Metropolitan University Japan DCB Test Simulation of Stitched CFRP Laminates Using Interlaminar Tension Test Results ThBM1-07
Naoyuki Watanabe Tokyo Metropolitan University Japan
Yutaka Iwahori Japan Aerospace Exploration Agency Japan
Toshio Nakamura State University of New York at Stony Brook USA INTERLAMINAR FATIGUE GROWTH UNDER THERMAL CYCLES IN COMPOSITE LAMINATE ThBM1-08
Narayanan Ramanujam State University of New York at Stony Brook USA
Pavankiran Vaddadi State University of New York at Stony Brook USA
Raman P Singh Oklahoma State University USA
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Thursday Afternoon (July 12) -- Room B-2: 14:20-18:20
Session Title: Delamination : Analysis II (Specialist Session)
Presenters Name Affiliation Country Paper Title pdf
Chairperson(s): TBD
Robin Olsson Imperial College London UK On Improper Foundation Models for the DCB Specimen ThBA1-01
Henk de Boer Advanced Lightweight Engineering Netherlands Modelling interfaces and bonded joints ThBA1-02
Jan-Jaap Koppert Advanced Lightweight Engineering Netherlands
Adriaan Beukers Delft University of Technology Netherlands
Harald Bersee Delft University of Technology Netherlands
Toshio Nagashima Sophia University Japan DELAMINATION PROPAGATION ANALYSIS OF COMPOSITE LAMINATE USING X-FEM ThBA1-03
Hiroshi Suemasu Sophia University Japan
Luis M. P. Durão ISEP - Engineering Superior Institute Porto Portugal Delamination analysis of carbon fibre reinforced laminates ThBA1-04
Antonio T. Marques University of Porto Portugal
Joao M. Tavares University of Porto Portugal
Antonio G. Magalhaes ISEP - Engineering Superior Institute Porto Portugal
Alessandro Airoldi Politecnico di Milano Italy Evaluation of numerical approaches for the development of interlaminar damage in composite laminates ThBA1-05
Giuseppe Sala Politecnico di Milano Italy
Session Title: Delamination : Application (Specialist Session)
Chairperson(s): Masaki Hojo
Ronald Krueger National Institute of Aerospace USA Panel-Stiffener Debonding Analysis Using A Shell/3D Modeling Technique ThBA2-01
James G. Ratcliffe National Institute of Aerospace USA
Pierre J. Minguet The Boeing Company USA
Jiye Chen University of Portsmouth UK PREDICTION OF DELAMINATION IN BRAIDED COMPOSITE T-PIECE SPECIMENS ThBA2-02
Eric Ravey University of Portsmouth UK
Stephen Hallett University of Portsmouth UK
Michael R. Wisnom University of Bristol UK
Matthew J. Hiley QinetiQ Ltd UK A Comparison of Through-Thickness Reinforcement Methods: Z-Pinning and Stitching ThBA2-03
Graeme Stringer QinetiQ Ltd UK
Yuichiro Aoki Japan Aerospace Exploration Agency Japan EFFECT OF DELAMINATION PROPAGATION ON MECHANICAL BEHAVIOR IN COMPRESSION AFTER IMPACT ThBA2-04
Hiroshi Kondo Tokai University Japan
Hiroshi Hatta Japan Aerospace Exploration Agency Japan
Aniello Riccio Italian Aerospace Research Center (CIRA) Italy INFLUENCE OF MATERIAL UNCERTAINTY ON THE DAMAGE RESISTANCE AND TOLERANCE OF STIFFEND COMPOSITE PANELS ThBA2-05
Marco Gigliotti Italian Aerospace Research Center (CIRA) Italy
T. Kevin O'Brien U.S. Army Research Laboratory USA Towards a Delamination Fatigue Methodology for Composite Materials ThBA2-06
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