Application of Infrared Stress Graphic System to Non-Destructive Evaluation of Composites

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概要

• 論文の詳細を見る
• 独立行政法人航空宇宙技術研究所の論文

著者

• Ishikawa Takashi

  Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi

• Sugimoto Sunao

  航空宇宙技術研究所

関連論文

• 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
• Experimental Examination of Theory of CTE (Coefficient of Thermal Expansion) Control Technology
• Application of Infrared Stress Graphic System to Non-Destructive Evaluation of Composites

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