Research theme for competitive and other funds (6):
2020 - 2025 Hypersonic Airframe/Engine Integration Experiment Using a Sounding Rocket FTB
2015 - 2018 極超音速複合サイクルエンジンの概念設計と極超音速推進性能の実験的検証
2015 - 2018 空気吸込式エンジンを搭載した極超音速実証機の機体/エンジン統合制御
2010 - 2012 Development of the dynamic simulator for the hypersonic turbojet engine including unsteady phenomena
2007 - 2009 Fundamental Research for Silent Supersonic Transport Based on Supersonic Biplane Theory
1.System Analysis of Hypersonic Transport Aircraft 2.System Analysis of Pre-Cooled Turbojet Engine
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Papers (21):
Manami Fujii, Shogo Ogura, Tetsuya Sato, Hideyuki Taguchi, Atsushi Hashimoto, Takashi Takahashi. Effect of angle of attack on the performance of the supersonic intake for High Mach Integrated Control Experiment (HIMICO). Aerospace Science and Technology. 2022. 127. 107687-107687
Shogo Ogura, Manami Fujii, Yusuke Hoshiya, Yuki Fujimori, Tetsuya Sato, Hideyuki Taguchi, Takayuki Kojima, Junichi Oki. Experimental study of high-speed air intake performance by side clearance. Aerospace Science and Technology. 2022. 123. 107439-107439
Masato Gokan, Mikiya Araki, Juan C. Gonzalez Palencia, Takayuki Kojima, Hideyuki Taguchi. Development of 1 MHz Class High Frequency Optical Microphone and Its Application to Jet Noise Reduction Device Performance Investigation. Journal of the Japan Society for Aeronautical and Space Sciences. 2022. 70. 1. 7-13
Tetsuya SATO, Hideyuki TAGUCHI, Takayuki KOJIMA, Takeshi TSUCHIYA, Mitsuhiro TSUE, Shinji NAKAYA, Akiko MATSUO, Asei TEZUKA, Takahiro FUJIKAWA, Koji MIYAJI. Program of High Mach Integrated Control Experiment, “HIMICO” Using S-520 Sounding Rocket. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 2021. 19. 6. 831-837