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

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA2120 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Shigeru Kuchiishi(kuchi-ishi.shigeru@jaxa.jp) Members: Shunji Enomoto, Junichi Kazawa, Atsushi Hashimoto, Takashi Ishida, Shigeru Kuchiishi, Mitsumasa Makida, Hiroki Ugajin, Taisuke Nambu, Manabu Hisida, Rika Yamada, Keiji Ueshima, Yuuhi Tanaka, Naoki Tani Abstract Unstructured-grid flow solver FaSTAR-Move and grid generator BOXFUN are applied to aero-engine elements with complicated configuration (such as linear and rotating・・・<<read more>>

Active Fluid Flow Control using DBD Plasma Actuators

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA1477 Subject Category: Aeronautical Technology PDF Responsible Representative: Yoshihisa Aoki, Aeronautical Technology Directorate, Aerodynamics Research Unit Contact Information: Yoshihisa Aoki(aoki@chofu.jaxa.jp) Members: Yoshihisa Aoki Abstract Improvement of aerodynamic characteristics using DBD plasma actuators. Reference URL N/A Reasons for using JSS2 It takes a lot of time to calcurate. Achievements of the Year Unsteady fluid flow analysis around cylinder was conducted using FaSTAR. Publications N/A Usage of JSS2 Computational Information Process Parallelization・・・<<read more>>

Aerodynamic Characteristics Improvement of Quad Tilt Wing VTOL Plane

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA0901 Subject Category: Aeronautical Technology PDF Responsible Representative: Yoshihisa Aoki, Aeronautical Technoloty Directorate, Aerodynamic Research Unit Contact Information: Yoshihisa Aoki(aoki@chofu.jaxa.jp) Members: Yoshihisa Aoki Abstract Aerodynamic characteristics improvement of Quad Tilt Wing VTOL plane in cruise. Reference URL Please refer to 'Four-engine tilt wing VTOL aircraft | Technology of VTOL/STOL | Aeronautical Technology Directorate'. Reasons for using JSS2 It takes a lot of time to calculate using workstation. Achievements of the・・・<<read more>>

Collarboration work on reseach and development for ecowing technology (future aircraft design)

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA0622 Subject Category: Aeronautical Technology PDF Responsible Representative: Yoshikazu Makino, Unit Head, Aeronautical Technology Directorate, Aviation Systems Research Unit Contact Information: morizawa@mech.tottori-u.ac.jp(morizawa@mech.tottori-u.ac.jp) Members: Seiichiro Morizawa, Keisuke Tokura Abstract For the future aircraft design, the aerodynamic characteristics of swept-back and swept-forward wings are compared using CFD. Through the parametric study of the planforms, the influences of the design parameters on the aerodynamic characteristics and flow fields are clarified. Reference URL N/A・・・<<read more>>

Environment Conscious Aircraft Systems Research in Eco-wing Technology: CFD Code Modifications

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JAXA Supercomputer System Annual Report April 2018-March 2019 Report Number: R18EA0621 Subject Category: Aeronautical Technology PDF Responsible Representative: Yoshikazu Makino, Unit Head, Aeronautical Technology Directorate, Aviation Systems Research Unit Contact Information: Mitsuhiro Murayama(murayama.mitsuhiro@jaxa.jp) Members: Yosuke Matsumura, Masayuki Kakehi, Mitsuhiro Murayama, Tomoaki Ikeda, Yasushi Ito Abstract In a research of environment-conscious aircraft systems resarch for environmental conscious aircraft technology named "Research for Eco-Wing technology", innovative drag reduction technologies are investigated to reduce the fuel consumption for a conventional aircraft configuration. Aircraft・・・<<read more>>