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 of Plasma Simulation in Electric Propulsion Devices

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22ECWU04 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Takashi Aoyama, Aviation Technology Directorate, Program Director Contact Information: Kiyoshi Kinefuchi, Department of Aerospace Engineering, Graduate School of Engineering, Nagoya University(kiyoshi.kinefuchi@mae.nagoya-u.ac.jp) Members: Fumito Takase, Ryohei Takagi Abstract The purpose of this research is to investigate the effect of the state of the lanthanum hexaboride insert responsible for thermal electron emission from the hollow cathode used as an electron source in・・・<<read more>>

Study on future space transportation system – combined cycle engine (JAXA-Tohoku Univ. collaborative course)

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22ECWU07 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Sadatake Tomioka, Associate Principal Researcher, Research and Development Directorate, 4th Unit. Contact Information: Sadatake Tomioka (RInsertHereD directorate, 4th Research Unit)(tomioka.sadatake@jaxa.jp) Members: Sadatake Tomioka, Hironobu Nishiguchi, Kota Kubosaki, Hattori, Ryota Ito, Shota Hatta Abstract Fully reusable launch vehicle will reduce the transportation cost and increase the space launch demands. Introduction of airbreathing engine will afford system weigth penalty necessary to realise・・・<<read more>>

Research on particle-grid hybrid analysis method

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22ECWU03 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Yasuhiro Mizobuchi, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Hiroki Tsujimura (Waseda University)(hiroki-tsujimura@toki.waseda.jp) Members: Hiroki Tsujimura Abstract In this project, we study the particle-grid hybrid analysis method, a novel method suitable for numerical analysis of liquid fuel atomization. In the method, liquid is calculated by a particle method (the moving particle simulation (MPS) method using JAXA’s software “P-flow”),・・・<<read more>>

Development of drag reduction technology for rotorcraft

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22ECMP23 Subject Category: Competitive Funding PDF Responsible Representative: Arizono Hitoshi, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub Contact Information: higo.ayumi@subaru.co.jp(higo.ayumi@subaru.co.jp) Members: Ayumi Higo, Tomofumi Iwamoto, Masafumi Sasaki, Hideaki Sugawara, Yasutada Tanabe Abstract 30% of the total drag of rotorcrafts is main rotor hub and mast drag. The hub fairing and the mast cowling were installed on the compound helicopter concept model developed by JAXA, and hub drag reduction effect・・・<<read more>>

Observational study on a free precession for a Magnetar.

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22ECMP24 Subject Category: Competitive Funding PDF Responsible Representative: Noriko Yamasaki, Institute of Space and Astronautical Science, Dept. of Space Astronomy and Astrophysics Contact Information: Nagomi Uchida(uchida.nagomi@jaxa.jp) Members: Nagomi Uchida Abstract Recently, pulse-phase modulations of X-ray pulsation are found from some strongly magnetized neutron stars (Magnetars). This can be interpreted as the presence of free precession and thus they are deformed to prolate spheroid. We verify these results with independently developed・・・<<read more>>