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Feedback Control of Flow Separation Using DBD Plasma Actuator

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EACA26 Subject Category: JSS Inter-University Research PDF Responsible Representative: Kengo Asada, Assistant Professor, Department of Information and Computer Technology, Faculty of Engineering, Tokyo University of Science Contact Information: Kengo Asada(asada@rs.tus.ac.jp) Members: Kengo Asada, Takuto Ogawa Abstract The project develops flow control technic by using dielectric barrier discharge (DBD) plasma actuator to establish high efficient and robust vehicle systems such as rockets, aircrafts, and motor vehicles. We propose and demonstrate feedback・・・<<read more>>

Investigation of internal flow of aircraft combustor for En-Core Project.

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA0714 Subject Category: Aeronautical Technology PDF Responsible Representative: Mitsumasa Makida(JAXA, Aeronautical Technology Directorate) Contact Information: Mitsumasa Makida(Aeronautical Technology Directorate)(makida.mitsumasa@jaxa.jp) Members: Mitsumasa Makida, Naoki Nakamura, Takashi Ishiyama Abstract In the development process of aircraft combustors, air mass flow distribution between fuel nozzles and cooling air holes on the liner effects performances of combustors. In this research, we conduct combustion simulations of internal flow inside the combustor which faithfully simulates the configuration・・・<<read more>>

Research on Structure and Composite Material Technologies for Digital Certification

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA1601 Subject Category: Aeronautical Technology PDF Responsible Representative: Yuichiro Aoki, Senior Researcher, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Yuichiro Aoki, Digital Structures and Materials Technology Team, Aircraft Lifecycle Innovation Hub, Aviation Technology Directorate(aoki.yuichiro@jaxa.jp) Members: Yuichiro Aoki, Yoshiyasu Hirano, Kenichi Kubota, Shintaro Kamiyama, Toshiyuki Kasahara, Hiroki Kawabe, Kasumi Nagao, Keita Nakamoto, Yasutomo Tateishi, Tetsuo Yasuoka Abstract The objective of this research is to accurately model manufacturing defects in・・・<<read more>>

Improvement of numerical analysis for internal flow with complicated configuration inside aero-engine

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA2120 Subject Category: Aeronautical Technology PDF Responsible Representative: ISHII Tatsuya, Director, Aviation Technology Directrate, Aviation Environmental Sustainability Innovation Hub Contact Information: Taisuke Nambu, Aviation Technology Directorate, Aviation Environmental Sustainability Innovation Hub(nambu.taisuke@jaxa.jp) Members: Kenji Hayashi, Junichi Kazawa, Takahisa Kohno, Taisuke Nambu, Hiroki Ugajin, Kanako Yasue Abstract Unstructured-grid flow solver FaSTAR-Move-AE are applied to aero-engine analysis with complicated configuration. Through the calculation, these programs are tested and investigated for the deficiency and・・・<<read more>>

Hydrogen Application to Aircraft and Future Space Transportation System

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EA2121 Subject Category: Aeronautical Technology PDF Responsible Representative: Sadatake Tomioka, Leader, Hydrogen Aerospace Plane Team Contact Information: Hideyuki Taguchi(taguchi.hideyuki@jaxa.jp) Members: Shima Ariyoshi, Manami Fujii, Motoyuki Hongoh, Yusuke Hoshiya, Daiki Ito, Yuki Kuwabara, Aoto Kikui, Shota Kiuchi, Masafumi Momose, Taisuke Nambu, Koutarou Nakayama, Koichi Omi, Naoyuki Okamura, Junichi Oki, Shunsuke Imamura, Takahiro Terao, Nozomi Takaki, Rintaro Tanaka, Hideyuki Taguchi, Kotaro Yamada Abstract This research aims at the demonstration of the thrust・・・<<read more>>