Shigeru Kuchiishi
Japan Aerospace Exploration Agency
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Featured researches published by Shigeru Kuchiishi.
52nd Aerospace Sciences Meeting | 2014
Shigeya Watanabe; Shigeru Kuchiishi; Keiichi Murakami; Atsushi Hashimoto; Hiroyuki Kato; Tatsuya Yamashita; Kanako Yasue; Kentaro Imagawa; Hideji Saiki; Jyun Ogino
The development of ‘Digital/Analog-Hybrid WINd tunnel (DAHWIN),’ which is an innovative system integrating CFD (Computational Fluid Dynamics) with EFD (Experimental Fluid Dynamics), is presented. The aim of DAHWIN is to improve efficiency, accuracy, and reliability of aerodynamic characteristics evaluation in aerospace vehicle developments through mutual support between EFD and CFD. DAHWIN is constructed as a system seamlessly connecting two large facilities, JAXA 2m x 2m Transonic Wind Tunnel for EFD and JAXA Supercomputer System for CFD. The function of this system consists of optimization of test planning, an accurate correction of the wind tunnel wall and support interaction effects, quasi-simultaneous monitoring of EFD data in comparison with corresponding CFD data, the most probable aerodynamic characteristics estimation based on both EFD and CFD data, and so forth. Each function is described with some examples of applications. Key technical challenges in the system development, such as an automatic grid generator, high-speed CFD solver, and a high-speed data processing technique for image measurement data, are also addressed. Some preliminary applications of DAHWIN to practical wind tunnel tests, such as civil transport tests, showed the usefulness and reliability of DAHWIN in terms of increasing efficiency and accuracy of both EFD and CFD.
Archive | 2005
Kazuo Sato; Tomoyuki Komuro; Hideyuki Tanno; Syuichi Ueda; Katsuhiro Itoh; Shigeru Kuchiishi; Shigeya Watanabe
Force measurement of a standard model HB-2 was performed in high enthalpy shock tunnel HIEST to study its aerodynamic characteristics. The force measurement results were compared with that obtained in conventional 1.27m hypersonic wind tunnel HWT1. The comparison showed that HIEST results agreed well with that of HWT1 in case of low enthalpy condition. The real gas effect on aerodynamic characteristics was also studied in case of high enthalpy condition.
Archive | 2011
Saki Kasamatsu; Takayuki Itoh; Shigeya Watanabe; Shigeru Kuchiishi; Kanako Yasue
Archive | 2005
Shigeru Kuchiishi; Shigeya Watanabe; Shinji Nagai; Shoichi Tsuda; Tadao Koyama; Noriaki Hirabayashi; Hideo Sekine; Koichi Hozumi; 口石 茂; 渡辺 重哉; 永井 伸治; 津田 尚一; 小山 忠勇; 平林 則明; 関根 英夫; 穂積 弘一
Archive | 2012
Kaori Hattanda; Takayuki Itoh; Shigeya Watanabe; Shigeru Kuchiishi; Kanako Yasue
JOURNAL OF THE FLOW VISUALIZATION SOCIETY OF JAPAN | 2006
Mitsuru Kurita; Kazunori Mitsuo; Shigeru Kuchiishi; Kazuyuki Nakakita; Shigeya Watanabe; Keisuke Fujii
33rd AIAA Fluid Dynamics Conference and Exhibit | 2003
Shigeru Kuchiishi; Shigeya Watanabe; Kazuyuki Nakakita; Tadao Koyama; Shuichi Ueda; Katsuhiro Itoh
2018 AIAA Aerospace Sciences Meeting | 2018
Kazuhisa Chiba; Yuhei Umeda; Naoki Hamada; Shinya Watanabe; Masaya Nakata; Kanako Yasue; Koji Suzuki; Takashi Atobe; Shigeru Kuchiishi; Kazuyuki Nakakita; Takeshi Ito
The Proceedings of Mechanical Engineering Congress, Japan | 2017
Kazuhisa Chiba; Shinya Watanabe; Masaya Nakata; Yuhei Umeda; Naoki Hamada; Kanako Yasue; Koji Suzuki; Shigeru Kuchiishi; Kazuyuki Nakakita; Takeshi Ito
Archive | 2017
Kazuhisa Chiba; Shinya Watanabe; Masaya Nakata; Yuhei Umeda; Naoki Hamada; Kanako Yasue; Koji Suzuki; Shigeru Kuchiishi; Kazuyuki Nakakita; Takeshi Ito; 一永 千葉; 真也 渡邉; 雅也 中田; 裕平 梅田; 直希 濱田; かな子 保江; 康司 鈴木; 茂 口石; 和之 中北; 健 伊藤