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Research and Development of Emission Free Aircraft Technologies

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA102H01 Subject Category: Aeronautical Technology PDF Responsible Representative: Akira Nishizawa, Aeronautical Technology Directorate Contact Information: Yuzuru Yokokawa(yokokawa.yuzuru@jaxa.jp) Members: Masaya Funada, Atsushi Hashimoto, Hiroshi Kobayashi, Taisuke Nambu, Takayuki Sakurai, Keisuke Sugaya, Yoshiharu Tamaki, Hirotaka Tsutsui, Keiji Ueshima, Kanako Yasue, Yuzuru Yokokawa Abstract With the ultimate goal of achieving emission-free (zero emissions) aircraft, research and development of electric hybrid propulsion system is conducted, which includes the WAT(Wake Adaptive Thruster) fans at the・・・<<read more>>

Application of the Cartesian grid and an IB method to the analysis of aircraft engine combustors

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA102G31 Subject Category: Aeronautical Technology PDF Responsible Representative: Daisuke Nambu, Contact Information: Taisuke Nambu, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub(nambu.taisuke@jaxa.jp) Members: Dan Hori, Manabu Hisida, Ryohei Kirihara, Takuya Karatsu, Takuhito Kuwabara, Yasuhiro Mizobuchi, Taisuke Nambu, Kei Shimura, Hiroki Yao, Satoshi Atsuchi, Naoki Tani Abstract Enabling to conduct numerical analysis of thermal fluid phenomena within aircraft engine combustors using HINOCA-AE ensuring reasonable TAT (Turn Around Time) and accuracy, the potential・・・<<read more>>

Aeroelastic Analysis for Rotocraft

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA102C21 Subject Category: Aeronautical Technology PDF Responsible Representative: Kanako, Yasue, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Hideaki Sugawara(sugawara.hideaki@jaxa.jp) Members: Keita Kimura, Hideaki Sugawara, Yasutada Tanabe Abstract The aeroelastic deformation of helicopter rotor blades affects the vibration and stability of the helicopter. The simulation technology is required to evaluate the aeroelastic deformation in the rotorcraft design. In this work, the research and development of aeroelastic analysis technology for・・・<<read more>>

CFD simulation of compound helicopter flight test

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA102C20 Subject Category: Aeronautical Technology PDF Responsible Representative: Kanako Yasue, Aviation Technology Directorate, team leader, Aircraft Life-cycle Innovation Hub, Airmobility Digital Design Team Contact Information: Keita Kimura(kimura.keita@jaxa.jp) Members: Yusuke Hamamoto, Fumihiro Kajiwara, Keita Kimura, Masahiko Sugiura, Hideaki Sugawara, Yasutada Tanabe Abstract JAXA has been conducting a research for the demonstration of a high-speed compound helicopter it has proposed, under various flight conditions. The high-speed compound helicopter is expected to fly・・・<<read more>>

Research on Airframe Noise Reduction Design (FQUROH-2)

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA101R21 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Program Director of Aviation Technology, Aviation Technology Directorate Contact Information: Takehisa Takaishi, FQUROH-2 Project Team (Airframe Noise Reduction Technology Project Team), Aviation Technology Directorate(takaishi.takehisa@jaxa.jp) Members: Takehisa Takaishi, Mitsuhiro Murayama, Yasushi Ito, Takashi Ishida, Yoimi Kojima, Kazuomi Yamamoto, Kentaro Tanaka, Tohru Hirai, Gen Nakano Abstract In order to meet the projected demand for air travel, strengthen the international competitiveness of Japan’s・・・<<read more>>