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 Airframe Noise Reduction Design (FQUROH-A)

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EDA101R21 Subject Category: Aeronautical Technology PDF Responsible Representative: Yasushi Watanabe, Program Director of Aviation Technology, Aviation Technology Directorate Contact Information: Takehisa Takaishi, Airframe Noise Reduction Team, Aviation Technology Directorate(takaishi.takehisa@jaxa.jp) Members: Takehisa Takaishi, Mitsuhiro Murayama, Yasushi Ito, Ryotaro Sakai, Kazuomi Yamamoto, Kazuki Fukaya, Kentaro Tanaka, Tohru Hirai, Gen Nakano, Takashi Ishida Abstract In order to meet the projected demand for air passengers, and to strengthen the international competitiveness of Japan airports・・・<<read more>>

Aerodynamic Simulations on Airframe Noise Reduction Technology (FQUROH-A)

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EDA101R20 Subject Category: Aeronautical Technology PDF Responsible Representative: Yasushi Watanabe, Program Director of Aviation Technology, Aviation Technology Directorate Contact Information: Takehisa Takaishi, Airframe Noise Reduction Team, Aviation Technology Directorate(takaishi.takehisa@jaxa.jp) Members: Takehisa Takaishi, Mitsuhiro Murayama, Yasushi Ito, Ryotaro Sakai, Kazuomi Yamamoto, Kazuki Fukaya, Kentaro Tanaka, Tohru Hirai, Gen Nakano, Takashi Ishida Abstract In order to meet the projected demand for air passengers, and to strengthen the international competitiveness of Japan airports・・・<<read more>>

Liquid-Propellant Propulsion System Simulation

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EG3215 Subject Category: Research and Development PDF Responsible Representative: Taro Shimizu, Research and Development Directorate, Research Unit III Contact Information: Hiedyo Negishi(negishi.hideyo@jaxa.jp) Members: Yu Daimon, Taroh Fukuda, Osamu Fukasawa, Ashvin Hosangadi, Hideyo Negishi, Takenori Nakajima, Shinji Ohno, Masashi Toyama, Andrea Zambon, Satoshi Ukai, Himeko Yamamoto, Rika Yamada Abstract Next generation of space transport systems need not only to reduce costs with high perfoemance propulsion for a particular mission but also・・・<<read more>>

Mars helicopter configuration and aerodynamical optimized blade

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21ECMP13 Subject Category: Competitive Funding PDF Responsible Representative: Yoshikazu Makino, Aeronautical Technology Directorate, Aviation Systems Research Unit Contact Information: Keita Kimura, JAXA(kimura.keita@jaxa.jp) Members: Yuta Buto, Keita Kimura, Masahiko Sugiura, Hideaki Sugawara, Kuniyuki Takekawa, Yasutada Tanabe, Kouta Yoshikawa Abstract A Mars helicopter “HAMILTON” has been developed by JAXA, Tokyo Metropolitan University and Kogakuin University. Since the atomospheric density on Mars is about 1/100, the sound of speed is about 3/4 compared・・・<<read more>>

Study of the Effect of Boundary Layer Ingestion (BLI) on Aircraft Propulsion

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EDA201P55 Subject Category: Aeronautical Technology PDF Responsible Representative: Keiichi OKAI, Associate Senior Researcher, Environmentally Sustainable Engine Team, Aviation Environmental Sustainability Innovation Hub, Aviation Technology Directorate Contact Information: Keiichi OKAI(okai.keiichi@jaxa.jp) Members: Keiichi Okai, Kazuhisa Amemiya, Tomoya Kogirima, Junichi Kazawa, Akiyoshi Masaki Abstract In this study, evaluation of unsteady aerodynamics in aircraft fan under strongly distorted inflow condition simulating airframe/engine integration configuration with Boundary Layer Ingestion (BLI) benefit suited for future electric・・・<<read more>>