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Aerodynamic optimal design of mars helicopter rotor blade planform

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20ECMP13 Subject Category: Competitive Funding PDF Responsible Representative: Keita Kimura, Aeronautial Technology Directorate, Aviation System Research Unit Contact Information: Keita Kimura(kimura.keita@jaxa.jp) Members: Yasutada Tanabe, Keita Kimura, Hideaki Sugawara, Kuniyuki Takekawa, Masahiko Sugiura Abstract Japan's own mission to investigate the inside of a pit crater on the surface of Mars is being considered for around 2030, and a helicopter capable of hovering is expected to play an active role because it・・・<<read more>>

Investigation on the structure of rotating detonation wave

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20ECMP12 Subject Category: Competitive Funding PDF Responsible Representative: Shingo Matsuyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Shingo Matsuyama(smatsu@chofu.jaxa.jp) Members: Shingo Matsuyama Abstract In this study, combustion analysis by large eddy simulation (Large-Eddy Simulation, LES) was carried out in order to clarify propagation characteristics and detailed structure of rotating detonation wave. Two-dimensional and three-dimensional simulations were carried out for stable operating conditions in the combustion test of the・・・<<read more>>

Research on rotor blade optimization between JAXA-ONERA-DLR : Validation of CFD solvers

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20ECMP11 Subject Category: Competitive Funding PDF Responsible Representative: Yasutada Tanabe, Aeronautical Technology Directorate, Aviation Systems Research Unit Contact Information: Keita Kimura(kimura.keita@jaxa.jp) Members: Yasutada Tanabe, Masahiko Sugiura, Hideaki Sugawara, Kuniyuki Takekawa, Keita Kimura Abstract In order to verify and accumulate knowledge of the analysis tools and optimization methods of helicopter blades possessed by JAXA, DLR, and ONERA, each organization has been optimizing blade shapes under various flight conditions. In this fiscal・・・<<read more>>

JAXA-SUBARU Cooperative Research

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20ECMP10 Subject Category: Competitive Funding PDF Responsible Representative: Yoshikazu Makino, Aeronautical Technology Directorate, Aviation Systems Research Unit Contact Information: Yasutada Tanabe(tan@chofu.jaxa.jp) Members: Yasutada Tanabe, Hideaki Sugawara, Masahiko Sugiura, Kuniyuki Takekawa, Masafumi Sasaki, Keita Kimura Abstract A compound helicopter is one of the high-speed rotorcraft concepts. Aerodynamic interactions occur on the winged compound helicopter, constructed by a single main rotor, winged-body, and multiple propellers. The drag of the rotorcraft drastically increases・・・<<read more>>

SGS Stress Transport Equation-based SGS Modeling for Comprehensive LES Model

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20ECMP08 Subject Category: Competitive Funding PDF Responsible Representative: Shingo Matsuyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Shingo Matsuyama(smatsu@chofu.jaxa.jp) Members: Shingo Matsuyama Abstract In this study, we aim to realize a comprehensive LES that does not require any tuning for model parameters to the target flow field by solving the SGS stress transport equations. The SGS stress equations are derived exactly from the spatial filtering operation, but requires・・・<<read more>>