Experiments and numerical analysis of compression after impact (CAI) behavior of CF/PIXA stiffened panels for HSCT structure
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概要
- 論文の詳細を見る
- 2005-09-01
著者
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ISHIKAWA Takashi
Advanced Composite Evaluation Technology Center, Japan Aerospace Exploration Agency (JAXA)
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Hayashi Yoichi
Japan Aerospace Technology Foundation 7-44-1 Jindaiji-higashi Machi Chofu-shi Tokyo 182 Japan
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MATSUSHIMA MASAMICHI
Advanced Composites Evaluation Technology Center, Japan Aerospace Exploration Agency
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HAYASHI YOICHI
Advanced Composites Evaluation Technology Center, Japan Aerospace Exploration Agency
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SCOTT MURRAY
Department of Aerospace Engineering, Royal Melbourne Institute of Technology
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Scott Murray
Department Of Aerospace Engineering Royal Melbourne Institute Of Technology
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Matsushima Masamichi
Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi
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Ishikawa Takashi
Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi
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Ishikawa Takashi
Advanced Composite Evaluation Technology Center Japan Aerospace Exploration Agency (jaxa)
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- Processing and properties of carbon fiber reinforced triple-A polyimide(Tri-A PI)matrix composites
- Effects of normal stress on the off-axis mechanical behavior of a plain-woven C/C composite
- Experiments and numerical analysis of compression after impact (CAI) behavior of CF/PIXA stiffened panels for HSCT structure
- Comparison of numerical analysis of linear and post-buckling behavior of CFRP T-stiffeners with experimental results
- ANALYSIS AND EXPERIMENTS OF POSTBUCKLING BEHAVIOR OF T-SHAPED CFRP STIFFENERS
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