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Numerical analysis on combustion instability considering spray response

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA201C30 Subject Category: Aeronautical Technology PDF Responsible Representative: Kenichiro Nagai, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub Contact Information: Kazuaki Matsuura, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub.(matsuura.kazuaki@jaxa.jp) Members: Kazuaki Matsuura, Yuta Sasaki, Kodai Kato, Yoshio Zama Abstract Numerical analysis on combustion instability considering spray response is performed to clarify phenomena and improve prediction capability of CFD in combustion instabilities.・・・<<read more>>

Numerical analysis for optimal design of helicopter rotor blades

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA201C22 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: Fumihiro Kajiwara, Keita Kimura, Masahiko Sugiura, Hideaki Sugawara, Yasutada Tanabe Abstract JAXA, DLR, and ONERA are collaborating on research as to blade optimization under various flight conditions for the purpose of validating and accumulating knowledge on the helicopter blade analysis tools and・・・<<read more>>

Optimal design of propellers for compound helicopters

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA201C21 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: Fumihiro Kajiwara, Keita Kimura, Masahiko Sugiura, Hideaki Sugawara, Ryo Takahashi, Yasutada Tanabe Abstract The objective of this study is to implement the optimal design of side and tail propellers for JAXA's proposed compound helicopter. The shapes are optimized to meet the design・・・<<read more>>

Aerodynamic Analysis for High-speed rotorcraft

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA201C20 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: Fumihiro Kajiwara, Yuki Kishi, Keita Kimura, Hideaki Sugawara, Ryo Takahashi, Yasutada Tanabe, Kanako Yasue Abstract Rotorcrafts have complex mechanisms around the main rotor and are exposed to non-streamlined shape parts, resulting in large aerodynamic drag. The aerodynamic drag of the hub accounts for 30% of the total drag・・・<<read more>>

Research on High Performance Control Surfaces and High Lift Devices

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JAXA Supercomputer System Annual Report February 2023-January 2024 Report Number: R23EDA201C18 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, Mitsuhiro Murayama Abstract The purpose of the research is to develop and mature a bunch of elemental technologies on aerodynamics, aeroacoustics, structures and sensing and system design technologies to achieve high perfromance control surfaces and・・・<<read more>>