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。

Robust design for Jet Engine/Aerodynamic performance analyses for LPT

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDA201C52 Subject Category: Aeronautical Technology PDF Responsible Representative: Atsushi Kanda, Aviation Technology Directorate, Aviation Environmental Sustainability Innovation Hub Contact Information: Junichi Kazawa, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub(kazawa.junichi@jaxa.jp) Members: Junichi Kazawa, Liki Matsuyama, Naoki Nakamura Abstract developing technologies that contribute to reducing losses in high-load LPT. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System The calculation is large-scale because it involves performing a stator-rotor-stator blade・・・<<read more>>

On-board clear-airturbulence prediction

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDA201D00 Subject Category: Aeronautical Technology PDF Responsible Representative: Tetsuya Nagashima, Aviation Technology Directorate, Aviation Safety Innovation Hub Contact Information: Tetsuya Nagashima(nagashima.tetsuya@jaxa.jp) Members: Ryuhei Daikatsu, Hirokazu Higashida, Tetsuya Nagashima, Takayuki Sakurai Abstract CAT (clear-air turbulence) simulations for research on on-board CAT prediction system. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System JSS is used to simulate the clear-air turbulence encountered by aircraft in weather analysis programmes. Achievements of・・・<<read more>>

Aerodynamics and Acoustics Simulations for Multiple Rotors

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDA201E10 Subject Category: Aeronautical Technology PDF Responsible Representative: Kanako Yasue, Aviation Technology Directorate, Aviation Integration Innovation Hub Contact Information: Hideaki Sugawara(sugawara.hideaki@jaxa.jp) Members: Isao Aozasa, Takuto Ohyama, Yuta Ozawa, Hideaki Sugawara, Hiroki Ura, Kanako Yasue Abstract This study investigates the improvement of aerodynamic performance and noise reduction in multirotor systems. Numerical simulations and wind tunnel experiments are conducted to investigate the fundamental mechanisms of aerodynamic interferences among multiple rotors and to・・・<<read more>>

Aeroelastic Analysis for Helicopter Rotor Blades

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDA201E20 Subject Category: Aeronautical Technology PDF Responsible Representative: Kanako Yasue, Aviation Technology Directorate, Aviation Integration Innovation Hub Contact Information: Hideaki Sugawara(sugawara.hideaki@jaxa.jp) Members: Tomoya Karasawa, Kohei Konishi, Hideaki Sugawara, Kazuma Tsujimura, Yuuka Tsurumaki, Shunsuke Takeuchi Abstract Aeroelastic deformation of helicopter rotor blades plays a significant role in vibration and noise generation. Accurate prediction of these effects through numerical simulation is essential in rotorcraft development. The objective of this study is to・・・<<read more>>

Technology demonstration of Airborne wind energy Kite system for Ordinary people

[Added on] [Last modified on]

JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDA201E77 Subject Category: Aeronautical Technology PDF Responsible Representative: Naoki Matayoshi, Aeronautical Technology Directorate Contact Information: Yoimi Kojima(kojima.yoimi@jaxa.jp) Members: Yoimi Kojima, Sho Yokoyama Abstract To reproduce the behavior of an aerial wind turbine kite on a flight simulator, we are analyzing the aerodynamic coefficient of the kite and the surrounding flow field during flight using CFD. The kite's characteristic behavior is a figure-eight flight due to self-excited oscillation, and we aim・・・<<read more>>