Ishikawa Takashi | Advanced Composite Evaluation Technology Center Japan Aerospace Exploration Agency (jaxa)
スポンサーリンク
概要
- Ishikawa Takashiの詳細を見る
- 同名の論文著者
- Advanced Composite Evaluation Technology Center Japan Aerospace Exploration Agency (jaxa)の論文著者
関連著者
-
ISHIKAWA Takashi
Advanced Composite Evaluation Technology Center, Japan Aerospace Exploration Agency (JAXA)
-
Ishikawa Takashi
Advanced Composite Evaluation Technology Center Japan Aerospace Exploration Agency (jaxa)
-
Ogasawara T
Advanced Composite Evaluation Technology Center Japan Aerospace Exploration Agency (jaxa)
-
Ogasawara Toshio
Advanced Composite Evaluation Technology Center National Aerospace Laboratory Of Japan
-
Ishikawa Takashi
Advanced Composite Evaluation Technology Center National Aerospace Laboratory Of Japan
-
OGASAWARA Toshio
Advanced Composite Evaluation Technology Center, Japan Aerospace Exploration Agency (JAXA)
-
OCHI Yasuo
University of Electro-Communications
-
Ogasawara Toshio
Advanced Composite Evaluation Technology Center Japan Aerospace Exploration Agency (jaxa)
-
Ochi Y
University Of Electro-communications
-
Zhu S
Univ. Tokyo
-
Zhu Shijie
Nagaoka University Of Technology
-
AOKI Takuya
Advanced Composite Evaluation Technology Center, Japan Aerospace Exploration Agency (JAXA)
-
Ogasawara Toshio
National Aerospace Laboratory of Japan
-
Ishikawa Takashi
National Aerospace Laboratory of Japan
-
Aoki T
Advanced Composite Evaluation Technology Center Japan Aerospace Exploration Agency (jaxa)
-
Ogasawara Toshio
National Aerospace Laboratory
-
Aoki Takuya
Advanced Composite Evaluation Technology Center Japan Aerospace Exploration Agency (jaxa)
-
Ishikawa Takashi
National Aerospace Laboratory
-
BESSHO Takayuki
University of Electro-Communications
-
Ohsawa Yutaka
University of Electro-Communications
-
Zhu Shijie
University of Electro-Communications
-
GOMYOU Takashi
University of Electro-Communications
-
ZHU Shijie
Institute of Industrial Science, University of Tokyo
-
Zhu Shijie
Institute Of Industrial Science University Of Tokyo
-
Ogasawara Toshio
Advanced Composite Evaluation Technology Center(ace-tec) National Aerospace Laboratory Of Japan(nal)
-
Miyagawa Kiyoshi
Ihi Aerospace Co. Ltd.
-
Yokota Rikio
Institute of Space and Astronautical Science
-
Yokota Rikio
Institute Of Space And Astronautical Science(isas)
-
Hayashi Yoichi
Japan Aerospace Technology Foundation 7-44-1 Jindaiji-higashi Machi Chofu-shi Tokyo 182 Japan
-
OZAWA HIDEKI
Ube Industries, Ltd.
-
TAGUCHI MITSUSHI
Ube Industries, Ltd.
-
SATO RYOUICHI
Ube Industries, Ltd.
-
SHIGENARI YU
IHI Aerospace Co., Ltd.
-
Shigenari Yu
Ihi Aerospace Co. Ltd.
-
Sato Ryouichi
Ube Industries Ltd.
-
MATSUSHIMA MASAMICHI
Advanced Composites Evaluation Technology Center, Japan Aerospace Exploration Agency
-
HAYASHI YOICHI
Advanced Composites Evaluation Technology Center, Japan Aerospace Exploration Agency
-
SCOTT MURRAY
Department of Aerospace Engineering, Royal Melbourne Institute of Technology
-
Scott Murray
Department Of Aerospace Engineering Royal Melbourne Institute Of Technology
-
Taguchi Mitsushi
Ube Industries Ltd.
-
Matsushima Masamichi
Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi
-
Ozawa Hideki
Ube Industries Ltd.
-
Ishikawa Takashi
Composite Structure Section Airframe Division National Aerospace Laboratory 6-13-1 Ohsawa Mitaka-shi
-
Ishikawa Takashi
Advanced Composite Evaluation Technology Center(ace-tec) National Aerospace Laboratory Of Japan(nal)
著作論文
- Transient Creep Behavior of a Plain Woven SiC Fiber/SiC Matrix Composite(Recent Advances in Materials and Processing (I))
- SB-05-2(041) Degradation of Tyranno^ZMI Fiber/Si-Ti-C-O Matrix Composites under Constant Load Conditions at Elevated Temperature(Ceramic, Polymer and Composites)
- High Temperature Fatigue Behavior of an orthogonal 3-D Woven SiC/Sic Composite
- 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