Comparison of numerical analysis of linear and post-buckling behavior of CFRP T-stiffeners with experimental results
スポンサーリンク
概要
著者
-
Hayashi Yoichi
Japan Aerospace Technology Foundation 7-44-1 Jindaiji-higashi Machi Chofu-shi Tokyo 182 Japan
-
MATSUSHIMA MASAMICHI
Advanced Composites Evaluation Technology Center, Japan Aerospace Exploration Agency
-
ISHIKAWA Takashi
Composite Structure Section, Airframe Division, National Aerospace Laboratory, 6-13-1 Ohsawa, Mitaka
-
MATSUSHIMA Masamichi
Composite Structure Section, Airframe Division, National Aerospace Laboratory, 6-13-1 Ohsawa, Mitaka
-
Matsushima Masamichi
Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi
-
Ishikawa Takashi
Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi
-
Ishikawa Takashi
Composite Structure Section Airframe Division National Aerospace Laboratory
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
- Numerical analysis of heat conduction effect corresponding to infrared stress measurements in multi-lamina CFRP