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Development of vortex generator layout design guidelines for improving aircraft performance by using vortex generators

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA201A01 Subject Category: Aeronautical Technology PDF Responsible Representative: Shigeru Hamamoto, Aerodynamics Research Unit, Aeronautical Technology Directorate Contact Information: Yasushi Ito, Aviation Systems Research Unit, Aeronautical Technology Directorate(ito.yasushi@jaxa.jp) Members: Yasushi Ito, Hiroya Toriida, Tohru Hirai Abstract The installation of vortex generators (VGs) in an aircraft is mainly used as a solution to problems that require performance improvement during the flight test phase, and its placement is often determined by trial and・・・<<read more>>

Research and Development of Emission Free Aircraft Technologies

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA102H01 Subject Category: Aeronautical Technology PDF Responsible Representative: Akira Nishizawa, Aeronautical Technology Directorate, Next Generation Aeronautical Innovation Hub Center Contact Information: Yuzuru Yokokawa(yokokawa.yuzuru@jaxa.jp) Members: Yuzuru Yokokawa, Hamidreza Kheirandish, Keiji Ueshima, Taisuke Nambu, Kanako Yasue, Atsushi Hashimoto, Hirotaka Tsutsui, Hiroshi Kobayashi Abstract This research and development treats a turbo-electric hybrid propulsion system and aircraft configuration for electrized systems, which aims at raising the technical maturity level of emission free aircrafts. Reference・・・<<read more>>

Flight Demonstration of LIDAR-based Gust Alleviation Control System

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA102H00 Subject Category: Aeronautical Technology PDF Responsible Representative: Atsushi Kanda,Hub Manager,Aeronautical Technology Directorate,Next Generation Aeronautical Innovation Hub Center Contact Information: Midori Maki(maki.midori@jaxa.jp) Members: Manabu Hisida, Midori Maki Abstract Flight demonstration of LIDAR-based Gust Alleviation Control System will be performed. CFD analysis was conducted to build an aerodynamic database for the demonstration aircraft. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System Objective: Building aerodynamic models for flight motion・・・<<read more>>

Digital tuft; measurement system of surface phisycal quantity for aircraft

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA102F00 Subject Category: Aeronautical Technology PDF Responsible Representative: Masaru 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>>

Nonlinear Aeroelastic Framework for Multi-fidelity Analysis

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EDA101S01 Subject Category: Aeronautical Technology PDF Responsible Representative: Hitoshi Arizono, Aeronautical Technology Directorate, Structures and Advanced Composite Research Unit Contact Information: Hitoshi Arizono(arizono.hitoshi@jaxa.jp) Members: Hitoshi Arizono, Youichi Sano, Natsuki Tsushima Abstract Nonlinear Aeroelastic Framework for Multi-fidelity Analysis Reference URL N/A Reasons and benefits of using JAXA Supercomputer System Because high fidelity analysis is very expensive for simulation Achievements of the Year We designed a wind tunnel test model by addtive・・・<<read more>>