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Numerical analysis on atomization and spray combustion

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EA2150 Subject Category: Aeronautical Technology PDF Responsible Representative: Tatsuya Ishii, Propulsion Research Unit, Aeronautical Technology Directorate Contact Information: Kazuaki Matsuura, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Propulsion Research Unit(matsuura.kazuaki@jaxa.jp) Members: Kazuaki Matsuura, Naoki Nakamura, Mitsumasa Makida, Huilai Zhang, Jun Iino, Kinya Saito Abstract A numerical study is performed to clarify phenomena on atomization and spray combustion. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System Phenomena on・・・<<read more>>

Numerical Analyses on Hypersonic Experimental Aircraft

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EA2121 Subject Category: Aeronautical Technology PDF Responsible Representative: Tatsuya Ishii, Unit Leader, Propulsion Technology Research Unit, Aeronautical Technology Directorate Contact Information: Hideyuki Taguchi(taguchi.hideyuki@jaxa.jp) Members: Motoyuki Hongoh, Hideyuki Taguchi, Hiroyuki Tanaka, Mizuki Fukazawa, Junichi Oki, Manami Fujii, Takahiro Terao, Koichi Omi, Kotaro Yoshihara, Koji Ikuma Abstract This research aims at the demonstration of the thrust control method of a hypersonic pre-cooled turbojet engine using liquid hydrogen fuel and the aircraft /・・・<<read more>>

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

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EA2120 Subject Category: Aeronautical Technology PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Taisuke Nambu, Aeronautical Technology Directorate, Numerical Simulation Research Unit(nambu.taisuke@jaxa.jp) Members: Shunji Enomoto, Junichi Kazawa, Atsushi Hashimoto, Takashi Ishida, Mitsumasa Makida, Hiroki Ugajin, Taisuke Nambu, Keiji Ueshima, Kanako Yasue, Takashi Aoyama, Kenji Hayashi Abstract Unstructured-grid flow solver FaSTAR-Move are applied to aero-engine analysis with complicated configuration. Through the calculation, these programs are・・・<<read more>>

Advanced simulation of internal flow in rotating machinery

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EA2111 Subject Category: Aeronautical Technology PDF Responsible Representative: Tatsuya Ishii, Aeronautical Technology Directorate, Propulsion Research Unit Contact Information: Junichi Kazawa, Aeronautical Technology Directorate, Propulsion Research Unit(kazawa.junichi@jaxa.jp) Members: Junichi Kazawa Abstract Implement LES and DES in the rotating coordinate system to improve the aerodynamic performance prediction accuracy of rotating machine like fan, compressor, and so on, flows by numerical simulation. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System・・・<<read more>>

Analytical study on stress concentration due to gap in AFP-manufactured laminates

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JAXA Supercomputer System Annual Report April 2020-March 2021 Report Number: R20EA1601 Subject Category: Aeronautical Technology PDF Responsible Representative: Toshiya Nakamura, Director, Aeronautical Technology Directorate, Structures and Advanced Composite Research Unit Contact Information: Yuichiro Aoki(aoki.yuichiro@jaxa.jp) Members: Yuichiro Aoki, Toshiyuki Kasahara, Hiroki Kawabe Abstract The aim of this study is to clarify the effect of manufacturing defects, such as gaps and overlaps, on the strength of CFRP laminates fabricated by automated fiber placement. Reference URL N/A Reasons and benefits of using JAXA・・・<<read more>>