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Noise suppression technology for aircraft jet engines

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JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EA0716 Subject Category: Aeronautical Technology PDF Responsible Representative: Tatsuya Ishii, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub Contact Information: Shunji ENOMOTO(enomoto.shunji@jaxa.jp) Members: Shunji Enomoto, Hideshi Oinuma, Kenichiro Nagai, Junichi Oki, Tatsuya Ishii Abstract Ultra high bypass ratio aviation jet engines have a smaller sound absorbing liner area than conventional engines. In this project, we will develop sound-absorbing device technology that provides high noise reduction performance even with a small-sized・・・<<read more>>

Multivariate time series data analysis

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JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EDA201N04 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: OHMICHI, Yuya(ohmichi.yuya@jaxa.jp) Members: Mami Hayakawa, Keita Nakamoto, Yuya Ohmichi, Kohmi Takahashi, Kento Yamada Abstract Knowledge extraction techniques for large datasets are important because the computers and numerical simulation techniques have been highly developed and they are producing a huge amount of data. In this study, we have been developing knowledge extraction・・・<<read more>>

Research on three-dimensional cavity flow

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JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21ECWU12 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Yuya ohmichi, Aeronautical Technology Directorate,Numerical Simulation Research Unit Contact Information: Yuya ohmichi (ohmichi.yuya@jaxa.jp) Members: Miumi Maezawa, Yuya Ohmichi Abstract It is well known that rectangular-shaped cavities, such as those found in aircraft landing gear storage areas, can cause noise due to self-excited oscillation caused by an unsteady fluid phenomenon. In this study, the phenomenon of self-excited oscillation inside cavities was・・・<<read more>>

Three-dimensional numerical simulation of discharge and flow related to airflow control using plasma actuator

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JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EACA16 Subject Category: JSS Inter-University Research PDF Responsible Representative: Naofumi Ohnishi, Professor, Tohoku University Contact Information: Naofumi Ohnishi(naohnishi@tohoku.ac.jp) Members: Naofumi Ohnishi, Shintaro Sato, Hideto Tamura Abstract Plasma actuator has attracted attention as a fluid control device using dielectric barrier discharge. In the experimental study, it has been pointed out that the discharge has a spanwise distribution of the electrode and has a three-dimensional structure. In this study, we perform the・・・<<read more>>

Multiphase Developed Turbulence Explored Using Numerical Simulations

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JAXA Supercomputer System Annual Report February 2021-January 2022 Report Number: R21EACA50 Subject Category: JSS Inter-University Research PDF Responsible Representative: Yutaro Motoori, Assistant Professor, Osaka University Contact Information: Yutaro Motoori (y.motoori.es@osaka-u.ac.jp) Members: Yutaro Motoori Abstract Turbulence is ubiquitous in many phenomena around us. Since turbulent flow mixes and diffuses mass rapidly, it is important to understand the transport phenomena by turbulence in many systems. In the present study, we reveal the transport mechanism of particles in fully developed inhomogeneous turbulence. For・・・<<read more>>