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Research on dynamic attitude stability evaluation of high-speed flying objects using CFD

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA60 Subject Category: JSS Inter-University Research PDF Responsible Representative: Koji Miyaji, Professor, Yokohma National University Contact Information: Koji Miyaji(miyaji@ynu.ac.jp) Members: Koji Miyaji, Hiromi Yahata Abstract Using Computational Fluid Dynamics (CFD), this study aims to evaluate the static and dynamic attitude stability of high-speed flying objects. In particular, our analysis focuses on the High-Mach Integrated Control experiment (HIMICO), which is being jointly developed by multiple universities with JAXA. We will utilize・・・<<read more>>

Numerical simulation towards clarification of control mechanism of nanosecond-pulsed-driven DBD plasma actuator

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA58 Subject Category: JSS Inter-University Research PDF Responsible Representative: Shintaro Sato, Assistant professor, Tohoku University Contact Information: Shintaro Sato(shintaro.sato.c3@tohoku.ac.jp) Members: Shintaro Sato, Hibiki Tomie Abstract Flow separation control in fluid machinery is important factor in terms of minimizing its energy loss. In particular, development of an active airflow control technique, that enhances the performance at off-design point, can dramatically improve the performance of fluid machinery. Plasma actuators have been attracted・・・<<read more>>

Low-cost rotary wing design applied to design optimization of roter blade for Mars helicopter

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA59 Subject Category: JSS Inter-University Research PDF Responsible Representative: Masahiro Kanazaki, Professor, Tokyo Metopolitan University Contact Information: Masahiro Kanazaki, Professor(kana@tmu.ac.jp) Members: Rikiya Hata, Nana Hasegawa, Masahiro Kanazaki, Takashi Matsuno, Taisei Nishimura Abstract In the exploration of Mars using helicopters and portable uncrewd drones on the Earth, fortable rotor blades are utilized, because they must be foldable and compact. A low-cost blade evaluation method based on blade element momentum theory has・・・<<read more>>

Aerodynamics of Re-entry Vehicle System with Inflatable Ballute

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA57 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 To determine the aerodynamic characteristics of a flight vehicle equipped with an inflatable ballute. In particular, the influence of the deformation of the ballute on the aerodynamic characteristics will be investigated. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System There have been・・・<<read more>>

Aerodynamics of Re-entry Capsule with Hyperbolic Contours

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EACA56 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 For deleveopment of future sample return capsule, we applied the hyperbolic contours to design the front shape of the capsue. To find the optimal shape of the capsule, we perfomed CFD analyses. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System There have・・・<<read more>>