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CFD Analysis of a Multiple Rotor UAV near Walls

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ECMP17 Subject Category: Competitive Funding PDF Responsible Representative: Yasutada Tanabe, Aeronautical Technology Directorate, Next Generation Aeronautical Innovation Hub Center Contact Information: Yasutada Tanabe tanabe.yasutada@jaxa.jp Members: Yasutada Tanabe, Hideaki Sugawara Abstract Represented by the multiple rotor type UAV (Unmanned Aerial Vehicle), or so-called drone, the flying robot has been applied to disaster relief and other operations. However, the wind and gust resistence of this type of drone need to be further・・・<<read more>>

Modal decomposition analysis of a flow field around a re-entry capsule

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ECMP20 Subject Category: Competitive Funding PDF Responsible Representative: Takashi Takahashi, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Yuya Ohmichi ohmichi.yuya@jaxa.jp Members: Yuya Ohmichi, Kenji Kobayashi Abstract Knowledge extraction techniques for large data sets are important because, recently, the computers and numerical simulation techniques have been highly developed and they produced massive datasets . In this study, we are developing knowledge extraction tools which extract patterns from a large・・・<<read more>>

SIP CFRP high fidelity modeling technology

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ECMP99 Subject Category: Competitive Funding PDF Responsible Representative: Yutaka Iwahori, Aeronautical Directorate, Structure and Advanced Composite Technology Reasearch Unit Contact Information: Akinori Yoshimura yoshimura.akinori@jaxa.jp Members: Akinori Yoshimura Abstract JAXA contributes to the SIP (Cross-ministerial Strategic Innovation Promotion) program, which is governed by Cabinet Office, Government of Japan. JAXA takes charge high fidelity modeling of the polymer matrix composites for aircraft structure. The calculation for the modeling is performed in this・・・<<read more>>

Research on the Future Transportation Technology ( Integrated Design of Airframe and Engine)

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EG3103 Subject Category: Research and Development PDF Responsible Representative: Kouichi Okita Research and Development Directorate, Unit IV Contact Information: Susumu Hasegawa hasegawa.susumu@jaxa.jp Members: Susumu Hasegawa Abstract The establishment of technologies for airframe/engine integration of the spaceplane for the realization of future space transportation technology. Reference URL N/A Reasons for using JSS2 The comparison between the experimental data obtained by wind tunnel tests and the numerical results were conducted and verified.・・・<<read more>>

Research for Future Transportation System (Research for Scramjet Engine Flow Path)

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EG3104 Subject Category: Research and Development PDF Responsible Representative: Koichi Okita, Research InsertHere Development Directorate, Reserch Unit 4 Contact Information: SATO Shigeru ssato@kakuda.jaxa.jp Members: Shigeru Sato, Toshihiko Munakata, Masaaki Fukui, Masaharu Takahashi Abstract The purpose is to investigate the influence of the internal flow path on the engine performance by help of CFD in the viewpoint of aerodynamics about a scramjet engine which is a main mode of combined cycle・・・<<read more>>