Rchr
J-GLOBAL ID：200901065520024487   Update date: Jan. 30, 2024

Kato Hiroyuki

カトウ ヒロユキ | Kato Hiroyuki
Affiliation and department：
Japan Aerospace Exploration Agency Aerodynamic Test Facility Team, Aeronautical Facility Research Unit, Aviation Technology Directorate

About Japan Aerospace Exploration Agency Aerodynamic Test Facility Team, Aeronautical Facility Research Unit, Aviation Technology Directorate


Job title： Chief Manager for Planning
Research field  (1)： Aerospace engineering
Research keywords  (2)： 粒子画像流速測定法 ,  Particle Image Velocimetry
Research theme for competitive and other funds  (4)：
  • 2015 - 2017 Investigation of interaction effect between a three-dimensional boundary layer and a streamwise vortex in a transonic flow using particle image velocimetry specialized for boundary layer measurement
  • 2010 - 2012 Fast responding pressure-sensitive paint: Accuracy improvement, combination with another measurement, and application to unsteady aerodynamics
  • 大型風洞における汎用PIVシステムの開発
  • Development of PIV System in Large-Scale Industrial Wind Tunnel
Papers (6)：
  • 野邑佑二, 亀田正治, 中北和之, 加藤裕之, 小池俊輔. Combined Measurement of Unsteady Pressure and Vorticity Fields of the Flow around a Cylinder by PSP and PIV. 可視化情報学会論文集(Web). 2015. 35. 4. 1-6
  • YAMAGUCHI Ginga, MATSUSHIMA Kisa, KATO Hiroyuki. Computational Experiment to Examine a Numerical Method of PIV Pressure Estimation for the Wake of a Wing Flying at Transonic Speed. SPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2015. 14. 85-94
  • SAWADA Hideo, HIGUCHI Hiroshi, KATO Hiroyuki, KUNIMASU Tetsuya. Non-Intrusive Measurements of a Blunt Circular Cylinder in a Magnetic Suspension Wind Tunnel. J. Wind Eng. 2008. 116. 115-120
  • HASHIMOTO Takuro, KATO Hiroyuki, WATANABE Shigeya. Techniques for Reducing Surface Halation in Stereoscopic PIV Measurement. Transactions of Visualization Society of Japan. 2005. 25. 1. 219-222
  • KOYAMA Tadao, WATANABE Shigeya, KATO Hiroyuki, SUZUKI Norio, NAKAKITA Kazuyuki. Quantitative Flow Visualization Techniques in the Aerospace Field. Transactions of Visualization Society of Japan. 2004. 24. 92. 23-29_1
ｍore...
MISC (31)：
  • 山田健翔, 内山貴啓, 加藤裕之, 上野真. Investigation Research on Potential Needs for Future Performance of Unmanned Fixed-Wing Aircraft. 宇宙航空研究開発機構研究開発資料 JAXA-RM-(Web). 2021. 20-003
  • 上野真, 香西政孝, 古賀星吾, 小池俊輔, 加藤裕之. Acquisition and Publication of Transonic Wind Tunnel Test Data of the 80% Scaled NASA Common Research Model. 日本航空宇宙学会年会講演会講演集(CD-ROM). 2018. 49th. 1. 2-2
  • 加藤裕之, 小池俊輔, 中北和之. 大型風洞における時系列PIV計測技術. 飛行機シンポジウム講演集(CD-ROM). 2016. 54th
  • MITSUO Kazunori, NAKAKITA Kazuyuki, KATO Hiroyuki, KUCHI-ISHI Shigeru, KURITA Mitsuru, URA Hiroki, MIZUNO Masahito, KOIKE Shunsuke. Large-scale Wind Tunnels at JAXA (2nd Part) : Advanced Aerodynamic Measurement Technology. Aeronautical and Space Sciences Japan. 2015. 63. 9. 293-300
  • 小池俊輔, 加藤裕之, 高間良樹, 徳川直子, 中北和之. JAXA2mx2m遷音速風洞における境界層PIV計測. 宇宙航空研究開発機構特別資料 JAXA-SP-. 2015. 14-011
ｍore...
Education (2)：
  • - 1997 Yokohama National University
  • - 1997 Yokohama National University Graduate School, Division of Engineering Department of Mechanical Engineering and Materials Science
Professional career (1)：
  • Doctor(Engineering) (Yokohama National University)
Association Membership(s) (7)：
可視化情報学会 ,  米国航空宇宙学会 ,  日本航空宇宙学会 ,  日本機械学会 ,  American Institute of Aeronautics and Astronautics ,  The Japan Society for Aeronautical and Space Sciences ,  The Japan Society of Mechanical Engineers
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