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Numerical Study on Ionization Structure and Shock Wave Propagation for Improving Flight Performance of Beaming Propulsion Vehcile

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA17 Subject Category: JSS Inter-University Research PDF Responsible Representative: Masayuki Takahashi, Associate Professor, Tohoku University Contact Information: Masayuki Takahashi, Tohoku University(masayuki.takahashi.c8@tohoku.ac.jp) Members: Koki Ito, Hiroyuki Suzuki, Soichiro Suzuki, Masayuki Takahashi Abstract In thus study, our objective is elucidating the ionization-front prpgation mechanism induced by high-power microwave in the microwave rocket. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System The use of JAXA supercomputer is required to conduct・・・<<read more>>

Three-dimensional numerical simulation of discharge and flow related to airflow control using plasma actuator

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA16 Subject Category: JSS Inter-University Research PDF Responsible Representative: Naofumi Ohnishi, Professor, Tohoku University Contact Information: Naofumi Ohnishi(naohnishi@tohoku.ac.jp) Members: Naofumi Ohnishi, Shintaro Sato Abstract Plasma actuator has attracted attention as a fluid control device using dielectric barrier discharge. In the experimental study, it has been pointed out that the discharge has a spanwise distribution of the electrode and has a three-dimensional structure. The three-dimensional structure affects the induced flow distribution・・・<<read more>>

Studies on nonlinear vortex dynamics in the later-stage of laminar-turbulent transition in compressible boundary layers

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA13 Subject Category: JSS Inter-University Research PDF Responsible Representative: Kazuo Matsuura, Associate Professor, Ehime University, Graduate School of Science and Engineering Contact Information: Kazuo Matsuura(matsuura.kazuo.mm@ehime-u.ac.jp) Members: Kazuo Matsuura Abstract In hypersonic transitional flows, there are many complicated factors such as density fluctuation and temperature fluctuation due to the co-existence of the region slower than the speed of sound and the region faster than the speed of sound inside the boundary・・・<<read more>>

Computational Study on Aerodynamic Characteristics of Reusable Slender Body Configurations

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA12 Subject Category: JSS Inter-University Research PDF Responsible Representative: Keiichi Kitamura, Associate Professor, Yokohama National University Contact Information: Tomohiro Mamashita(mamashita-tomohiro-nj@ynu.jp) Members: Yuka Hara, Hibiki Kumai, Keiichi Kitamura, Tomohiro Mamashita, Kouya Nakahara Abstract Reusable launch vehicles are studied to reduce space transportation costs. Reusable rockets perform return flights that conventional expendable rockets do not experience. We worked to clarify the aerodynamic characteristics of a vehicle during the return phase using numerical・・・<<read more>>

Numerical Simulations of Fully Developed Turbulence

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA05 Subject Category: JSS Inter-University Research PDF Responsible Representative: Susumu Goto, Professor, Osaka University Contact Information: Susumu Goto(s.goto.es@osaka-u.ac.jp) Members: Ryo Araki, Hideto Awai, Susumu Goto, Kenta Hayashi, Wataru Iwashita, Yusuke Koide, Shota Kukimoto, Napat Lilittrakul, Yutaro Motoori, Hideki Murahata, Satoshi Matsumoto, Hayato Masuda, Gendai Nakano, Akito Oda, Masahiro Suzuki, Tomoki Sekigawa, Kodai Saheki, Hiroya Tanioka, Daiki Watanabe, Kiwamu Yoshii Abstract Most of flows around us are turbulence, and their prediction・・・<<read more>>