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Investigation of Aerodynamic Performances at Low Reynolds Number Condition with Mach Number Effect

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EACA18 Subject Category: JSS Inter-University Research PDF Responsible Representative: Seiichiro Morizawa, Lecturer, National Institute of Technology, Okinawa College Contact Information: Seiichiro Morizawa(morizawa@okinawa-ct.ac.jp) Members: Seiichiro Morizawa, Takashi Matsuno Abstract Birds such as hawks have excellent characteristics of flight efficiency and quiteness. One of these distingusished features is thought to be the shape of wingtip with multiple wings and gaps. The purpose of this project is to clarify these mechanisims of wingtip・・・<<read more>>

Numerical Simulation on Ionization Structure and Shock Wave Propagation for Flight-performance Improvement of Beaming Propulsion Vehicle

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EACA17 Subject Category: JSS Inter-University Research PDF Responsible Representative: Masayuki Takahashi, Associate Professor, Tohoku University Contact Information: Masayuki Takahashi(mtakahashi@rhd.mech.tohoku.ac.jp) Members: Masayuki Takahashi Abstract To achieve a better design of beaming propulsion vehicle, we numerically reproduce propagation processes of beam-supported plasma and shock wave by simulation and evaluate beam-power dependence on discharge-structure and propagation speed. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System A conputational cost becomes huge・・・<<read more>>

Discharge-flow coupling simulation towards airflow control using nanosecond-pulse-driven plasma actuators

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EACA16 Subject Category: JSS Inter-University Research PDF Responsible Representative: Naofumi Ohnishi, Professor, Tohoku University Contact Information: Naofumi Ohnishi(ohnishi@rhd.mech.tohoku.ac.jp) Members: Naofumi Ohnishi, Shintaro Sato Abstract Dielectric barrier discharge (DBD) plasma actuators are promising devices as active airflow control. The purpose of this project is to clarify the mechanism of flow separation control around an airfoil using DBD plasma actuators driven by repetitive nanosecond pulses in terms of discharge-flow coupling simulation. Reference・・・<<read more>>

Computational Study on Aerodynamic Characteristics of Reusable Slender Body Configurations

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EACA12 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: Keiichi Kitamura, Tomohiro Mamashita Abstract In this study, we are attempting to predict the aerodynamic characteristics of the reusable experimental vehicle “RV-X” with a two-stage cone by both wind tunnel tests and numerical analysis in preparation for its flight test. In the previous study, the validity of the numerical・・・<<read more>>

Construction of LES model for high-Mach-number multiphase turbulent flows based on DNS

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EACA11 Subject Category: JSS Inter-University Research PDF Responsible Representative: Kota Fukuda, Assistant Professor, Department of Aeronautics and Astronautics, Tokai University Contact Information: Kota Fukuda Tokai University(fukuda@tokai-u.jp) Members: Kota Fukuda, Taku Nonomura, Takayuki Nagata Abstract Direct Numerical Simulation (DNS) of the flow around a single particle in a compressible low Reynolds number flow is performed to understand the high Mach number solid-gas mixed phase turbulence, and the effect of the presence・・・<<read more>>