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Numerical study on low-speed buffet

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18ETET26 Subject Category: Skills Acquisition System PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Masashi Kanamori(kanamori.masashi@jaxa.jp) Members: Masashi Kanamori, Takahiro Yoshikawa Abstract It is of a great importance to predict a so-called low-speed buffet phenomenon for realizing safer flight. During a flight with a high angle-of-attack condition in a low-speed regime, separated flow at a leading edge of main wing impinges on its tail,・・・<<read more>>

Research for Aircraft Aeroacoustic Noise Prediction Technologies

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18ETET27 Subject Category: Skills Acquisition System PDF Responsible Representative: Yoshikazu Makino, Aviation Systems Research Unit, Aeronautical Technology Directorate Contact Information: Ryotaro Sakai(sakai.ryotaro@jaxa.jp) Members: Christian Nauck Abstract Innovative drag reduction technologies are investigated to reduce the fuel consumption for a conventional aircraft configuration. Aircraft noise prediction technologies and the conceptual design technologies are also developed for future aircraft which achieve low noise and high efficiency. In this research, aeroacoustic simulations have・・・<<read more>>

Research on aircraft engine combustor simulation

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18ETET23 Subject Category: Skills Acquisition System PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Rui Toyonaga(toyonaga.l.0121@ruri.waseda.jp) Members: Rui Toyonaga Abstract For the development of a aircraft engine combustor with high environmental compatibility, we develop the combustion calculation method that can reproduce the pressure propagation and chemical reaction with practical calculation cost. In addition, a verification calculation of this calculation method is conducted on the・・・<<read more>>

CFD simulations of a wind turbine wake for rapid recovery of velocity deficits

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18ETET09 Subject Category: Skills Acquisition System PDF Responsible Representative: Yasutada Tanabe, Leader, High Speed Rotorcraft Research Section Aviation Systems Research Unit Aeronautical Technology Directorate Contact Information: The University of Tokyo, Keita Kimura(k.kimura@ilab.eco.rcast.u-tokyo.ac.jp) Members: Keita Kimura, Yasutada Tanabe Abstract In a large wind farm (arrays of wind turbines), wind turbine wake can cause power deficits or/and additional fatigue in turbine stands in wake region. In this study, several wake simulations were・・・<<read more>>

Basic research for system integration of silent supersonic airplane technologies

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18ETET01 Subject Category: Skills Acquisition System PDF Responsible Representative: Yoshikazu Makino, Aeronautical Technology Directorate, Aviation Systems Research Unit Contact Information: Yoshikazu Makino (makino.yoshikazu@jaxa.jp) Members: Yuki Kishi, Go Iwamoto, Masahiro Kanazaki, Yoshikazu Makino, Hideyuki Obata, Yuki Sato, Nao Setoguchi, Hidekazu Yoshida, Toshiya Yokoi Abstract The system integration design technologies for achieving low sonic-boom, low aerodynamic drag, low landing and take-off noise, and light weight simultaneously are the key technologies for future・・・<<read more>>