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aFJR high efficiency fan technology development

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2710 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, Shunji Enomoto, Toshio Nishizawa, Susumu Kato, Kenshi Yamashita 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. To compensate for increasing fan diameter, we・・・<<read more>>

aFJR light weight sound absorption liner technology development

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2740 Subject Category: Aeronautical Technology PDF Responsible Representative: Toshio Nishizawa, Aeronautical Technology Directorate, aFJR project team Contact Information: Shunji ENOMOTO enomoto.shunji@jaxa.jp Members: Shunji ENOMOTO, Tatsuya ISHII, Daisuke Sasaki, Hidemi Toh, Tsubasa Iwafune, Yusuke Akamisaka, Takuma Kanda, Ryo Inagaki, Hitoshi Morita 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・・・<<read more>>

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>>