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aFJR Lightweight low-pressure turbine technology development

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2750 Subject Category: Aeronautical Technology PDF Responsible Representative: Toshio Nishizawa, aFJR Project Team, Aeronautical Technology Directorate Contact Information: Junichi Kazawa kazawa.junichi@jaxa.jp Members: Junichi Kazawa, Toshio Nishizawa, Yasuo Horiguchi Abstract The purpose of aFJR project is to advance research on jet engine component technologies so that Japanese manufacturers can join more effectively in international joint-development projects on next-generation jet engines. In order to suppress the weight increase of the low pressure・・・<<read more>>

Numerical investigation of combustible flows using the adaptive mesh refinement (AMR)

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EACA35 Subject Category: JSS2 Inter-University Research PDF Responsible Representative: Edyta Dzieminska, Department of Engineering and Applied Sciences, Faculty of Science and Technology, Sophia University Contact Information: Edyta Dzieminska Edyta.d@sophia.ac.jp Members: Edyta Dzieminska, Yuta Aishima, Kota Sato, Yuto Hara, Mitsuharu Morishita, Hajime Sakai, Yuichi Niga, Syota Yamamoto, Xinmeng Tang Abstract We mainly do the investigations the behaviors of combustible flows, especially H2/Air and H2/O2 mixtures with high or normal pressures. The・・・<<read more>>

Active Fluid Flow Control using DBD Plasma Actuators

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA1477 Subject Category: Aeronautical Technology PDF Responsible Representative: Shigeru Hamamoto, Aeronautical Technology Directorate, Aerodymics 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 times to calculate using workstation. Achievements of the Year Unsteady fluid flow analysis around cylinder was conducted using FaSTAR. Publications N/A Usage of JSS2 Computational・・・<<read more>>

Research of Advanced Rotorcraft

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ECMP11 Subject Category: Competitive Funding PDF Responsible Representative: Yasutada Tanabe, Aeronautical Technology Directorate, Next Generation Aeronautical Innovation Hub Center Contact Information: Masahiko Sugiura sugiura.masahiko@jaxa.jp Members: Yasutada Tanabe, Masahiko Sugiura, Hideaki Sugawara Abstract Research on advanced technologies of aircraft (helicopter) is conducted to construct and validate an optimization design tool. Reference URL Please refer to 'Future type rotary-airfoil airplane system technology | Sky Frontier – Sky Frontier Program | Aeronautical Technology・・・<<read more>>

Study on Future Space Transportation System using Air-breathing Engines

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EG3205 Subject Category: Research and Development PDF Responsible Representative: Kouichi Okita, Research and Development Directorate, Research Unit 4 Contact Information: Masatoshi Kodera kodera.masatoshi@jaxa.jp Members: Masahiro Takahashi, Masatoshi Kodera, Masaaki Fukui, Toshihiko Munakata, Masaharu Takahashi, Sadatake Tomioka, Akihiro Shimuta, Takuto Miyaura Abstract Recently, reusable rockets have been being studied to reduce the cost of space transportation systems significantly. However, in order to extend the structural lifetime, it is necessary to operate・・・<<read more>>