本文へ移動

サイトナビゲーションへ移動

検索ボックスへ移動

サイドバーへ移動

ここは、本文エリアの先頭です。

Research on High Performance Control Surfaces and High Lift Devices

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EECOLE Subject Category: Aeronautical Technology PDF Responsible Representative: Dongyoun Kwak, Aviation Enviromental Sustanability Innovation Hub, Aviation Technology Directorate Contact Information: Mitsuhiro Murayama, Aviation Environmental Sustainability Innovation Hub, Aviation Technology Directorate(murayama.mitsuhiro@jaxa.jp) Members: Ryutaro Furuya, Yasushi Ito, Junichi Kazawa, Mitsuhiro Murayama Abstract The purpose of the research is to develop and mature a bunch of elemental technologies on aerodynamics, aeroacoustics, and structures and system design technologies to achieve high perfromance control surfaces・・・<<read more>>

Lunar near-surface thermal modelling

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EEE20101 Subject Category: Space Exploration PDF Responsible Representative: YAMAMOTO Mitsuo, Lunar and Planetary Exploration Data Analysis Group (JLPEDA) Contact Information: YAMAMOTO Mitsuo, Lunar and Planetary Exploration Data Analysis Group (JLPEDA)(yamamoto.mitsuo@jaxa.jp) Members: Shinichi Kinoshita, Risa Miyazaki, Hiroyuki Sato, Kenta Tanaka, Mitsuo Yamamoto Abstract Because observational data do not provide the required spatial and temporal resolutions, we aim to develop a simulation model to predict lunar near-surface temperatures at higher resolution. Reference・・・<<read more>>

CFD and CFD-DEM coupled simulation for a large-scale PSI test

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EEE21100 Subject Category: Space Exploration PDF Responsible Representative: Kota Tanabe, JAXA Space Exploration Center, Space Exploration System Technology Unit Contact Information: Mitsuhisa Baba(baba.mitsuhisa@jaxa.jp) Members: Mitsuhisa Baba, Arnaud Delibie Abstract There is a risk that during spacecraft take-off and landing, large amounts of regolith will be scattered from the ground by the engine exhaust plume and that craters will be formed. We will develop technology to properly assess this risk and・・・<<read more>>

Numerical Simulation on Hypersonic Boundary Layer

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EEG60100 Subject Category: Research and Development PDF Responsible Representative: Shuto Yatsuyanagi, Research and Development Directorate, Research Unit IV Contact Information: Shuto Yatsuyanagi(yatrsuyanagi.shuto@jaxa.jp) Members: Shuto Yatsuyanagi Abstract Hypersonic boundary-layer transition is a critical phenomenon in the design of atmospheric reentry vehicles and hypersonic cruise aircraft. At sufficiently high Reynolds numbers, the boundary layer undergoes transition from laminar to turbulent flow. Since the wall heat flux and skin friction in a turbulent・・・<<read more>>

Aerodynamic analysis of Japan's next generation primary launch vehicle

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EEG60101 Subject Category: Research and Development PDF Responsible Representative: Hideaki Nanri, Director of Research Unit 4, Research and Development Directorate, Research Unit 4 Contact Information: Hideaki Ogawa(ogawa.hideaki@jaxa.jp) Members: Fumihiro Itoo, Mizuki Murakami, Yukinori Morita, Takuya Ogura, Minoru Yoshimoto, Hideaki Ogawa Abstract Japan's next generation primary launch vehicle which reuses the first stage is being studied in order to reduce the space transportation cost drastically. The aerodynamic characteristics in the reentry・・・<<read more>>

ここは、サイドバー・エリアの先頭です。

News - Recent Posts

JSS3を利用するには / How to use JSS3

JSS3 を利用するには 「利用するには 」ページをご覧ください。
To use JSS3, please refer to "How to use JSS3" page.