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Development of 3D CFD core-software of automotive engine combustion chamber

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201N11 Subject Category: Aeronautical Technology PDF Responsible Representative: MIZOBUCHI Yasuhiro, Senior researcher, Aeronautical echnology Directrate, Numerical Simulation Research Unit Contact Information: MIZOBUCHI Yasuhiro, Japan Aerospace Exploration Agency, Aeronautical Technology Directrate(mizo@chofu.jaxa.jp) Members: Taisuke Nambu, Hiroki Yao, Shogo Yasuda, Yasuhiro Mizobuchi, Hiroyuki Abe, Manabu Hisida, Atsusi Fujino, Daichi Obinata, Takuhito Kuwabara, Shintaro Koike, Mikiroh Motoe, Kei Shimura, Toshikuni Koganei Abstract Enhancement of CAE utilization in automotive engine research by developing an engine・・・<<read more>>

High-Resolution, Efficient CFD Methods by Second Slope Limiter for Transonic Speeds

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201N10 Subject Category: Aeronautical Technology PDF Responsible Representative: Keiichi Kitamura, Yokohama National University, Faculty of Engineering, Division of Systems Research Contact Information: Keiichi Kitamura(kitamura@ynu.ac.jp) Members: Atsushi Hashimoto, Keiichi Kitamura, Masashi Kanamori, Hayato Kawashima, Yoshikatsu Furusawa, Takuma Yamaguchi, Fumiya Tsutsui, Yuya Yasumura, Tomohiro Mamashita, Kazuki Kakizaki, Shogo Motoki, Kiyokaze Okayama, Hirokazu Kurihara, Kaede Makino, Daichi Ishdo Abstract A high-resolution, Delayed DES has been conducted around whole the aircraft under the low-speed・・・<<read more>>

Investigation of Indirect Reynolds Number Effect

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201N08 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Director, Numerical Simulation Research Unit, Aeronautical Technology Directorate Contact Information: Makoto Ueno, Numerical Simulation Research Unit, Aeronautical Technology Directorate (ueno.makoto@jaxa.jp) Members: Wataru Yamazaki, Hiroki Ichihashi, Makoto Ueno Abstract We investigated and examined measures to improve the method of reproducing the loss considered to be equivalent to the tripping roughness of forced transition of the boundary layer of the wind tunnel・・・<<read more>>

Development of combustor simulation system based on physics understanding and modelling

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201N06 Subject Category: Aeronautical Technology PDF Responsible Representative: AOYAMA Takashi, Director, Aeronautical Technology Directrate, Numerical Simulation Research Unit Contact Information: MIZOBUCHI Yasuhiro(mizo@chofu.jaxa.jp) Members: Manabu Hisida, Taisuke Nambu, Hiroki Yao, Shogo Yasuda, Yasuhiro Mizobuchi, Hiroyuki Abe, Takeshi Okabe, Shingo Matsuyama, Mikiroh Motoe, Kazuya Uchiyama, Kei Shimura, Yoichi Ohnishi, Tetsuji Ogawa, Takuhito Kuwabara Abstract Development of simulation technology applicable to combustor design based on physics understanding and modelling by detailed and high-fidelity・・・<<read more>>

Systematic improvement of build and comparison of aerodynamic models of aircraft

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201N05 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Director, Numerical Simulation Research Unit, Aeronautical Technology Directorate Contact Information: Makoto Ueno, Numerical Simulation Research Unit, Aeronautical Technology Directorate (ueno.makoto@jaxa.jp) Members: Makoto Ueno, Yuko Ueno, Kento Yamada, Hiroya Toriida, Takahiro Uchiyama, Masaru Naruoka, Tetsujiro Ninomiya Abstract A research to realize efficient validation of numerical simulation using experimental data such as flight test and wind tunnel test data utilizing mathematical model.・・・<<read more>>