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Analysis and high-efficiency control of unsteady aerodynamic phenomena based on simultaneous measurement of pressure, temperature, position, and deformation

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22ECMP19 Subject Category: Competitive Funding PDF Responsible Representative: Kazuyuki Nakakita, Aviation Technology Directorate, Aircraft Lifecycle Innovation Hub Contact Information: Yoimi Kojima(kojima.yoimi@jaxa.jp) Members: Masato Imai, Kohei Konishi, Kazuyuki Nakakita, Yoimi Kojima, Keita Ogura, Hideaki Sugawara, Takumi Yumino Abstract We will establish a method for simultaneous measurement of pressure, temperature, position, and deformation for flow around a wing, and use this method to elucidate unsteady aerodynamic phenomena around airfoils with elastic deformation・・・<<read more>>

En-Core Project / High Precision Analysis for Turbine Blade

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EBA30313 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Ymane, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project Contact Information: Junichi Kazawa, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project(kazawa.junichi@jaxa.jp) Members: Junichi Kazawa Abstract We will contribute to strengthening international competitiveness by demonstrating technologies for high-temperature, high-efficiency turbines and ultra-low NOx lean burn combustors that reduce nitrogen oxide (NOx) and CO2 emissions. Reference URL・・・<<read more>>

Study of combustion instability

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22ECMP16 Subject Category: Competitive Funding PDF Responsible Representative: Seiji Tsutsumi, Research and Development Directorate, Research Unit III Contact Information: Seiji Tsutsumi(tsutsumi.seiji@jaxa.jp) Members: Junya Aono, Hiroyuki Ito, Noriyasu Omata, Seiji Tsutsumi Abstract In this study, LS-FLOW-HO was used to conduct a two-dimensional LES analysis of Continuously Variable Resonant CoContinuously Variable (CVRC) with varying inlet oxidizer temperature. Then, the database with and without combustion instability was generated. We will develop a reduced・・・<<read more>>

En-Core Project / Turbine aerodynamic performance analysis

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EBA30311 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Ymane, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project Contact Information: Junichi Kazawa, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project(kazawa.junichi@jaxa.jp) Members: Yasuo Horiguchi, Susumu Kato, Junichi Kazawa Abstract We will contribute to strengthening international competitiveness by demonstrating technologies for high-temperature, high-efficiency turbines and ultra-low NOx lean burn combustors that reduce nitrogen oxide (NOx) and・・・<<read more>>

En-Core Project / Turbine internal cooling analysis

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JAXA Supercomputer System Annual Report February 2022-January 2023 Report Number: R22EBA30312 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Ymane, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project Contact Information: Junichi Kazawa, Aeronautical Technology Directorate, En-Core (environmentally compatible core engine technology research) project(kazawa.junichi@jaxa.jp) Members: Susumu Kato, Junichi Kazawa, Yoji Okita Abstract We will contribute to strengthening international competitiveness by demonstrating technologies for high-temperature, high-efficiency turbines and ultra-low NOx lean burn combustors that reduce nitrogen oxide (NOx) and・・・<<read more>>