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

July/10 (Tue.) -- Room H

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

July/10(Tue.) -- Room A / B-2 / F / G / H / I / J / K

Tuesday Morning (July 10) -- Room H: 9:20-14:20
Session Title: Damage Tolerance, Imapct and Compression after Impact Behavior (Specialist Session)
Name Affiliation Country Paper Title pdf
Organizers Nobuo Takeda The University of Tokyo Japan
Takashi Ishikawa Japan Aerospace Exploration Agency Japan
Chairperson(s): Nobuo Takeda
Keynote Robert L. Sierakowski Air Force Research Laboratory USA DAMAGE TOLERANCE ISSUES FOR COMPOSITE MATERIALS TuHM1-01
Olesya I Zhupanska University of Florida, REEF USA LOW VELOCITY IMPACT OF ELECTRIFIED CARBON FIBER POLYMER MATRIX COMPOSITES TuHM1-02
Igor Y Telichev University of Florida, REEF USA
Robert L Sierakowski Air Force Research Laboratory USA
Opukuro S. David-West University of Strathclyde UK A STUDY OF REPEATED IMPACT LOADING ON A SYMMETRICAL CARBON FIBRE LAMINATE TuHM1-03
David H Nash University of Strathclyde UK
William M Banks University of Strathclyde UK
Akinori Yoshimura The University of Tokyo Japan CHARACTERIZATION OF OUT-OF-PLANE IMPACT DAMAGE IN STITCHED CFRP LAMINATES TuHM1-04
Tomoaki Nakao The University of Tokyo Japan
Nobuo Takeda The University of Tokyo Japan
Shigeki Yashiro National Institute of Advanced Industrial Science and Technology (AIST) Japan
Chairperson(s): Richard Butler
Sandor Becz ABAQUS, Inc. USA Analysis of Barely Visible Impact Damage for Aerospace Structures TuHM1-05
Eric Lapczyk ABAQUS, Inc. USA
Juan Hurtado ABAQUS, Inc. USA
Alex B Harman DSTO Australia Damage tolerance and impact resistance of composite scarf joints TuHM1-06
Chun Hui Wang DSTO Australia
Robin Olsson Imperial College London UK Experimental Validation of Delamination Criterion for Small Mass Impact TuHM1-07
Jifeng Xu Boeing Phantom Works USA MODELING HAIL IMPACT DAMAGE AND RESIDUAL STRENGTH IN COMPOSITE STRUCTURES TuHM1-08
Abe Askari Boeing Phantom Works USA
Olaf Weckner Boeing Phantom Works USA
Stewart Silling Sandia National Laboratories USA
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Tuesday Afternoon (July 10) -- Room H: 14:20-18:40
Session Title: Damage Tolerance, Imapct and Compression after Impact Behavior (Specialist Session)
Name Affiliation Country Paper Title pdf
Chairperson(s): Nobuhide Uda
Andrew D Foreman QinetiQ UK AN INTEGRATED SYSTEM FOR IMPROVED DAMAGE RESISTANCE AND LIGHTNING STRIKE PROTECTION IN COMPOSITE STRUCTURES TuHA1-01
Tahera Nensi QinetiQ UK
Paul T Curtis DSTL UK
Hiroshi Kondo Tokai University Japan Residual indentation,delamination area and CAI strength of CFRP laminates under low-velocity impact TuHA1-02
Katsumi Hiraoka Tokai University Japan
Yuichiro Aoki Japan Aerospace Exploration Agency Japan
Hiroshi Hatta Japan Aerospace Exploration Agency Japan
Hiroshi Suemasu Sophia University Japan COMPRESSIVE BEHAVIOR OF IMPACT DAMAGED COMPOSITE LAMINATES TuHA1-03
Wataru Sasaki Sophia University Japan
Yuuichiro Aoki Japan Aerospace Exploration Agency Japan
Takashi Ishikawa Japan Aerospace Exploration Agency Japan
Richard Butler University of Bath UK Compressive Strength of Impact Damaged Laminates TuHA1-04
Andrew T Rhead University of Bath UK
Giles W Hunt University of Bath UK
Yuichiro Aoki Japan Aerospace Exploration Agency Japan EFFECTS OF WATER ABSORPTION AND TEMPERATURE ON COMPRESSION AFTER IMPACT (CAI) STRENGTH OF CFRP LAMINATES TuHA1-05
Ken Yamada MAZDA Motor Corporation Japan
Takashi Ishikawa Japan Aerospace Exploration Agency Japan
Chairperson(s): Hiroshi Suemasu
Nobuhide Uda Kyushu University Japan Compression Fatigue Failure of CFRP Laminates with Impact Damage TuHA2-01
Kousei Ono Kyushu University Japan
Kazumi Hirano National Institute od Advanced Industrial Science and Technology (AIST) Japan COMPARISONS OF DAMAGE TOLERANCE BETWEEN POST-IMPACT FATIGUE AND OPEN-HOLE FATIGUE FOR HIGH TEMPERATURE POLYMER MATRIX COMPOSITES TuHA2-02
Takeshi Takatoya Japan Aerospace Exploration Agency Japan COMPRESSION AFTER IMPACT PROPERTIES OF HYBRID COMPOSITE MATERIALS TuHA2-03
Yutaka Sato Japan Aerospace Exploration Agency Japan
Ippei Susuki Japan Aerospace Exploration Agency Japan
Naohito Tsuda Japan Aircraft Development Corporation Japan
Adrian F. Gill Imperial College London UK Measurement of damage progression in open hole tension tests TuHA2-04
Paul Robinson Imperial College London UK
Dennis Hitchings Imperial College London UK
Julien Rion Ecole Polytechnique Fédérale de Lausanne Swiss Damage analysis of ultralight composite sandwich structures TuHA2-05
Yves Leterrier Ecole Polytechnique Federale de Lausanne Swiss
Fabio Demarco Ecole Polytechnique Federale de Lausanne Swiss
Jan-Anders Manson Ecole Polytechnique Federale de Lausanne Swiss
Shi-dong Pan Harbin Institute of Technology China INVESTIGATION OF FAILURE BEHAVIOR IN HONEYCOMB SANDWICH PANEL CONTAINING INTERFACIAL DEBONDING TuHA2-06
Lin-zhi Wu Harbin Institute of Technology China
Shan-Yi Du Harbin Institute of Technology China
Mohammad Reza Khoshravan University of Tabriz Iran Numerical Modeling of Delamination in Woven Composites TuHA2-07
Farzin Azimpoor University of Tabriz Iran
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