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Development of low cost rotor blade evaluation method and its application to Mars helicopter rotor blade

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EACA59 Subject Category: JSS Inter-University Research PDF Responsible Representative: Masahiro Kanazaki, Professor, Tokyo Metropolitan University Contact Information: Masahiro Kanazaki, Professor, Tokyo Metropolitan University(kana@tmu.ac.jp) Members: Rikiya Hata, Nana Hasegawa, Masahiro Kanazaki, Daisuke Kikuchi, Yuki Kishi, Takashi Matsuno, Takuya Nankaku, Taisei Nishimura Abstract In the exploration of Mars using helicopters and portable unmanned drones on the Earth, multi-rotor types with smaller aspect ratios of rotor blades are utilized, because they must be・・・<<read more>>

ALOS-2 / PALSAR-2 data processing for the entire observation period

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EAR10600 Subject Category: Space Technology PDF Responsible Representative: Sobue Shin-ichi,Associate Chief office of Earth Observation Missions,Space Technology Directorate I Contact Information: Kudoh fumio(kudoh.fumio@jaxa.jp) Members: Risako Dan, Daisuke Fukai, Takashi Goto, Naoyoshi Hirade, Kouji Hagiwara, Hidetoshi Hayasaka, Osamu Isoguchi, Koichi Imamura, Ryou Inami, Takashi Ikeda, Shun Ito, Fumio Kudoh, Yusuke Kobayashi, Hirotaka Kurokawa, Yasuhiro Kawashima, Yota Makinae, Shunsuke Murakami, Masahiro Murata, Nobuhiro Muramoto, Taroh Mutoh, Hidekazu Mikai, Toshimi Nakata, Katsuyuki Otsuka,・・・<<read more>>

Aerodynamics of Re-entry Capsule with Hyperbolic Contours

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EACA56 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: Masaya Nagasawa, Hirotaka Otsu, Ryoga Tsujimoto 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・・・<<read more>>

Aerodynamics of Re-entry Vehicle System with Inflatable Ballute

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EACA57 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: Shinichiro Mekata, 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・・・<<read more>>

Investigation of the effect of slow gas heating on nanosecond-pulse-driven plasma actuators

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EACA58 Subject Category: JSS Inter-University Research PDF Responsible Representative: Shintaro Sato, Assistant professor, Tohoku University Contact Information: Shintaro Sato(satoshin@rhd.mech.tohoku.ac.jp) Members: Shintaro Sato, Hibiki Tomie Abstract Flow separation control in fluid machinery is an important factor in terms of energy loss. Vortex generators, for example, can suppress separation, but they work only under specific conditions. Active flow control is required to function under a variety of conditions. In recent years, the・・・<<read more>>