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Development of 3D CFD core-software of automotive engine combustor

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA1937 Subject Category: Aeronautical Technology PDF Responsible Representative: Yasuhiro Mizobuchi, Aeronautical Technology Directrate, Numerical Simulation Research Unit Contact Information: Yasuhiro Mizobuchi mizo@chofu.jaxa.jp Members: Taisuke Nambu, Hiroki Yao, Shogo Yasuda, Yuichi Matsuo, Yasuhiro Mizobuchi, Hiroyuki Abe, Manabu Hisida, Jin Kusaka, Akira Kikusato, Tsukasa Hori, Youichi Ogata, Yoshimitsu Kohashi, Atsusi Fujino, Shun Ito, Daichi Obinata, Jun Hashimoto, Ryohei Kirihara, Takuhito Kuwabara, Yasushi Noguchi, Kazuhiro Uehara, Taisuke Kayashima, Yurina Maeda, Hiroyuki Sakai, Chikara・・・<<read more>>

Development and application of two-phase flow solver around moving objects

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA10 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Shun Takahashi, Tokai University Contact Information: Shun Takahashi takahasi@tokai-u.jp Members: Shun Takahashi Abstract Two-phase flows with moving objects are commonly used in practical engineering products. This study is subject to investigate the effect of the micro particles in the exhausted gas from the rocket engine to the strong pressure waves and the thermal conductance modification due to the water film around・・・<<read more>>

Computational Simulations for Aircraft Modification Design in the FQUROH Project

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2800 Subject Category: Aeronautical Technology PDF Responsible Representative: Kazuomi Yamamoto, FQUROH Project Team, Aeronautical Technology Directorate Contact Information: Kazuomi Yamamoto yamamoto.kazuomi@jaxa.jp Members: Kazuomi Yamamoto, Yasushi Ito, Takehisa Takaishi, Mitsuhiro Murayama, Ryotaro Sakai, Tohru Hirai, Kentaro Tanaka, Kazuhisa Amemiya, Gen Nakano, Takashi Ishida Abstract The FQUROH project aims at raising the technical maturity level of the noise reduction technology for high-lift devices and landing gear, which draws international attention to reduce・・・<<read more>>

Construction of LES Model for High Mach-number-turbulent-multi-phase-flow model based on DNS

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA11 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Kota Fukuda, Tokai University Contact Information: Kota Fukuda fukuda@tokai-u.jp Members: Kota Fukuda Abstract In order to construct LES model for high Mach number multi-phase turbulent flow, direct numerical simulation (DNS) of high Mach number and low Reynolds number flow around a particle will be carried out and construction of its data base and examination of the flow phenomena will be conducted.・・・<<read more>>

Computational Study on Aerodynamic Characteristics of Slender Body Configurations

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA12 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Keiichi Kitamura, Gaduate School of Engineering, Yokohama National University Contact Information: Takuya Aogaki aogaki-takuya-rf@ynu.jp Members: Keiichi Kitamura, Takuya Aogaki, Yuya Takagi Abstract We conducted numerical analysis on a slender body configuration which mimics a reusable rocket. In this study, we acquired detailed flowfields which have not been obtained from previous experiments and related them with aerodynamic characteristics. We also investigated and・・・<<read more>>