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Development of combustor simulation system based on physics understanding and modelling

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JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA201N06 Subject Category: Aeronautical Technology PDF Responsible Representative: AOYAMA Takashi, Director, Aeronautical Technology Directrate, Numerical Simulation Research Unit Contact Information: MIZOBUCHI Yasuhiro(mizo@chofu.jaxa.jp) Members: HISHIDA Manabu, NAMBU Taisuke, YAO Hiroki, YASUDA Shogo, MATSUO Yuichi, MIZOBUCHI Yasuhiro, ABE Hiroyuki, OKABE Takeshi, MATSUYAMA Shingo, MOTOE Mikiroh, UCHIYAMA Kazuya, SHIMURA Kei Abstract Development of simulation technology applicable to combustor design based on physics understanding and modelling by detailed and high-fidelity simulations Reference URL Please・・・<<read more>>

Systematic improvement of build and comparison of aerodynamic models of aircraft

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JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA201N05 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Makoto Ueno, JAXA(ueno.makoto@jaxa.jp) Members: Makoto Ueno, Hiroya Toriida, Yuko Ueno Abstract A research to realize efficient validation of numerical simulation using experimental data such as flight test and wind tunnel test data utilizing mathematical model. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System It is necessary to perform・・・<<read more>>

Digital tuft; measurement system of surface phisycal quantity for aircraft

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JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA102F00 Subject Category: Aeronautical Technology PDF Responsible Representative: Msasru Naruoka, Aeronautical Technology Directorate, Flight Research Unit Contact Information: Masaru Naruoka(naruoka.masaru@jaxa.jp) Members: Masaru Naruoka, Hiroya Toriida Abstract Development of measurement system of surface phisycal quantity for aircraft Reference URL N/A Reasons and benefits of using JAXA Supercomputer System The puropose is to perform CFD analyses for estimation of aerodynamic penalty of aircraft equipped with the developed sensor system. The advantage of・・・<<read more>>

Cooperative Research on Airframe Noise Reduction Technology (FQUROH+) #2

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JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA101R26 Subject Category: Aeronautical Technology PDF Responsible Representative: Kazuomi Yamamoto, FQUROH+ Team, Aviation Systems Research Unit, Aeronautical Technology Directorate Contact Information: Kazuomi Yamamoto(yamamoto.kazuomi@jaxa.jp) Members: Shinsuke Nishimura, Yuki Morisaki, Kazuomi Yamamoto, Yasushi Ito, Mitsuhiro Murayama, Ryotaro Sakai Abstract This collaborative research is being carried out as part of the FQUROH (Flight Demonstration of Quiet Technology to Reduce Noise from High-Lift Configurations) project aimed at raising the technical maturity level of the・・・<<read more>>

Cooperative Research on Airframe Noise Reduction Technology (FQUROH+) #1

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JAXA Supercomputer System Annual Report April 2019-March 2020 Report Number: R19EDA101R25 Subject Category: Aeronautical Technology PDF Responsible Representative: Kazuomi Yamamoto, FQUROH+ Team, Aviation Systems Research Unit, Aeronautical Technology Directorate Contact Information: Kazuomi Yamamoto(yamamoto.kazuomi@jaxa.jp) Members: Kazuhide Isotani, Yousuke Ueno, Hidemasa Yasuda, Yuta Tsuchimoto, Kazuomi Yamamoto, Yasushi Ito, Mitsuhiro Murayama, Ryotaro Sakai Abstract This collaborative research is being carried out as part of the FQUROH (Flight Demonstration of Quiet Technology to Reduce Noise from High-Lift Configurations) project aimed at raising the technical・・・<<read more>>