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Design optimization of distributed micro plasma actuators for flow control

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EACA47 Subject Category: JSS Inter-University Research PDF Responsible Representative: Takashi Matsuno, Associate Professor, Tottori University Contact Information: Takashi Matsuno(matsuno@tottori-u.ac.jp) Members: Masahiro Kanazaki, Seiichiro Morizawa, Takashi Matsuno, Taisei Takagi Abstract Plasma actuators (PAs) are flow control devices that generate wall jets on smooth surfaces using discharge plasma and have high potential for aerodynamic applications. The objective of this project is to establish application and optimization methodologies for PAs to realize transition・・・<<read more>>

Study of compressibility effect on low-Reynolds-number flow over a airfoil

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EACA49 Subject Category: JSS Inter-University Research PDF Responsible Representative: Taku Nonomura, Professor, Nagoya University Contact Information: Taku Nonomura (Professor at Nagoya University)(nonomura@nagoya-u.jp) Members: Taku Nonomura, Takayuki Nagata, Naotaka Shigeta, Yuri Sato, Tentaro Uchida Abstract Large-eddy simulations (LES) are performed under compressible conditions of flow around symmetric airfoils, including flat plates with Reynolds numbers of O(10^3)-O(10^4), to elucidate the effects of compressibility on laminar separation bubbles and turbulent transition. In the・・・<<read more>>

Numerical analysis of internal flow fields in aerospace propulsion systems over a wide operating range

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EACA52 Subject Category: JSS Inter-University Research PDF Responsible Representative: Shinichiro Ogawa, Assistant professor, Osaka Metropolitan University Contact Information: Shinichiro Ogawa, Assistant professor, Osaka Metropolitan University(shinichiro.ogawa@omu.ac.jp) Members: Shinichiro Ogawa, Haruyuki Kato, Daisuke Sasaki Abstract In this project, a three-dimensional computational fluid dynamics (CFD) solver based on the Building-Cube Method (BCM) is developed to enable accurate and efficient analysis of complex flow fields within aerospace propulsion systems. Conventional CFD solvers face challenges・・・<<read more>>

Study of particle Mach number and temperature effects on shock-particle interaction

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EACA55 Subject Category: JSS Inter-University Research PDF Responsible Representative: Takayuki Nagata, Assistant Professor, Nagoya University Contact Information: Takayuki Nagata (Assistant Professor at Nagoya University)(nagata.takayuki.x7@f.mail.nagoya-u.ac.jp) Members: Taku Nonomura, Takayuki Nagata, Shunta Takahashi Abstract This study focuses on compressible multiphase flows and investigates particle-laden flows and flows around small particles through direct numerical simulation of the Navier–Stokes equations. The objective is to acquire fundamental knowledge for understanding high-speed particle-laden flow phenomena, such・・・<<read more>>

Aerodynamics of Re-entry Vehicle System with Inflatable Ballute

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EACA57 Subject Category: JSS Inter-University Research PDF Responsible Representative: Hirotaka Otsu, Professor, Ryukoku University Contact Information: Hirotaka Otsu, Professor, Ryukoku University(otsu@rins.ryukoku.ac.jp) Members: Hirotaka Otsu Abstract We will investigate the aerodynamic characteristics of a flying vehicle equipped with a deployable parachute. In particular, we will use fluid-structure interaction analysis to examine the effect of parachute deformation on aerodynamic performance. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System In・・・<<read more>>

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