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Anyoji Masayuki Last modified date:2020.08.31

Associate Professor / Interdisciplinary Graduate School of Engineering Sciences
Department of Advanced Environmental Science and Engineering
Faculty of Engineering Sciences


Graduate School
Undergraduate School


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Homepage
https://kyushu-u.pure.elsevier.com/en/persons/masayuki-anyoji
 Reseacher Profiling Tool Kyushu University Pure
Phone
092-583-7583
Academic Degree
Ph.D in Engineering
Country of degree conferring institution (Overseas)
No
Field of Specialization
Experimental Gas Dynamics, Fluid Measurement
Total Priod of education and research career in the foreign country
00years01months
Research
Research Interests
  • Fluid image analysis using optical flow for high velocity impinging jet
    keyword : Impinging jet, image analysis, optical flow
    2017.04.
  • Application of Global Skin Friction meter to fluid analysis around vehicle body
    keyword : Global Skin Friction meter, Luminescent oil, Ahmed body, Aerodynamics
    2017.04.
  • Development of high performance wing at low Reynolds numbers
    keyword : low Reynolds number, mars airplane, high performance wing
    2015.04.
  • Development of Surface Skin Friction Measurement Technique
    keyword : Skin friction, Non-contact, Luminescent oil-film skin-friction meter
    2014.04.
  • Shock wave oscillation in two dimensional C-D nozzle
    keyword : supersonic, shock wave, jet flow, acoustic
    2014.10~2018.03.
  • Aerodynamic Characteristics of a Mars Airplane
    keyword : Mars Airplane, Low Reynolds Number, Aerodynamic Performance, Wind Tunnel Test
    2011.04~2014.03.
  • Development of a Mars Wind Tunnel and Its Applications to Low Reynolds Number and High-subsonic Airfoil Testing
    keyword : Mars Wind Tunnel, Mars Airplane, Low Reynolds Number Flow, Compressibility, Similarity Rule
    2008.04~2011.03.
Academic Activities
Papers
1. Katsuya Kajiwara, Masayuki Anyoji, Turbulence Intensity Effects on a Leading-Edge Separation Bubble of Flat Plate Wing at Low-Reynolds Numbers, Journal of Flow Control, Measurement & Visualization, accepted for publication, 2020.08.
2. M. Hijikuro,M. Anyoji, Application of Optical Flow Analysis to Shadowgraph Images of Impinging Jet, Journal of Flow Control, Measurement & Visualization, accepted for publication, 2020.07.
3. M. Anyoji, D. Hamada, High-Performance Airfoil with Low Reynolds-Number Dependence on Aerodynamic Characteristics, Fluid Mechanics Research International Journal, Vol.3, Issue 3, 76-80, 2019.08.
4. H. Aono, K. Kondo, T. Nonomura, M. Anyoji, A. Oyama, K. Fujii, M. Yamamoto, Aerodynamics of owl-like wing model at low Reynolds numbers, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, accepted for publication, 2019.07.
5. M. Anyoji, S. Wakui, D. Hamada, H. Aono, Experimental Study of Owl-like Airfoil Aerodynamics at Low Reynolds Numbers, Journal of Flow Control, Measurement & Visualization, 10.4236/jfcmv.2018.63015 , 6, 3, 185-197, 2018.07.
6. Yuta Ozawa, Taku Nonomura, Masayuki Anyoji, Hiroya Mamori, Naoki Fukushima, Akira Oyama, Kozo Fujii, Makoto Yamamoto, Identification of Acoustic Wave Propagation Pattern of a Supersonic Jet Using Frequency-Domain POD, Transactions of the JSASS, 61, 6, pp. 281-284, 2018.04.
7. M. Anyoji, M. Okamoto, K. Fujita, H. Nagai, A. Oyama, Evaluation of Aerodynamic Performance of Mars Airplane in Scientific Balloon Experiment, Fluid Mechanics Research International Journal, 1, 3, 2017.11.
8. M. Anyoji, I. Tabaru, Effect of Boundary Layer Trip on Reduction of Jet Noise in Over-Expanded Nozzle Flow, Journal of Thermal Science, Vo. 26, No. 5, 1-5, 2017.09.
9. Donghwi Lee, Soshi Kawai, Taku Nonomura, Masayuki Anyoji, Hikaru Aono, Akira Oyama, Keisuke Asai, Kozo Fujii, Mechanisms of surface pressure distribution within a laminar separation bubble at different Reynolds numbers, Physics of Fluids, 10.1063/1.4913500, 27, 2, 023602, 2015.02.
10. Masayuki Anyoji, Daiu Numata, Hiroki Nagai, Keisuke Asai, Pressure-Sensitive Paint Technique for Surface Pressure Measurement in a Low Density Wind Tunnel, Journal of Visualization, 10.1007/s12650-014-0239-9, Vol. 18, Isuue 2, pp. 297-309, 2014.10.
11. Masayuki Anyoji, Daiju Numata, Hiroki Nagai, Keisuke Asai, Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows, AIAA Journal, 10.2514/1.J053468, Vol. 53, Issue 6, pp. 1640-1654, 2015.05, The effects of Reynolds number, Mach number, and gas species (air andCO2) on aerodynamic characteristics of a thin flat plate and a NACA 0012-34 airfoil were investigated under low-Reynolds-number (Re ! 0:43 × 104 to 4.1 × 104) and high-subsonic-flow (M ! 0.1 to 0.6) conditions. In addition to lift and drag measurements by a two component balance system, the pressure-sensitive paint technique was applied to measure pressure profiles on the model surface. For the flat plate, the Reynolds number moderately affects the lift and drag characteristics because of asimple behavior of the leading-edge separation bubble; the length of the separation bubble increases as the angle of attack increases. By contrast, the Mach number and specific heat ratio contribute little to the aerodynamicperformance. For the NACA 0012-34 airfoil, the lift curves are highly dependent on the Reynolds number because of the formation, shift, and burst of the separation bubble, whereas the compressibility affects only the stall characteristics. The specific heat ratio has little effect on the aerodynamic performance. In common for both airfoils,it was observed that the Mach-number effect allows for the delay of a laminar–turbulent transition and reattachmentof the separated shear layer..
12. M. Anyoji, T. Nonomura, H. Aono, A. Oyama, K. Fujii, H. Nagai, K. Asai, Computational and Experimental Analysis of a High Performance Airfoil under Low-Reynolds Number Flow Condition, Journal of Aircraft, 10.2514/1.C032553, Vol. 51, No. 6, pp.1864-1872, 2014.12.
13. M. Anyoji, M. Okamoto, H. Hidaka, K. Kondo, A. Oyama, H. Nagai, K. Fujii, Control Surface Effectiveness of Low Reynolds Number Flight Vehicles, Journal of Fluid Science and Technology, 10.1299/jfst.2014jfst00XX, Vol.9, No.5, No. 14-00176, 2014.11.
14. M. Anyoji, M. Okamoto, H. Hidaka, T. Nonomura, A. Oyama, K. Fujii, Planetary Atmosphere Wind Tunnel Tests on Aerodynamic Characteristics of a Mars Airplane Scale Model, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 12, ists29, Pk_7-Pk_12, 2014.01.
15. M. Anyoji, K. Nose, S. Ida, D. Numata, H. Nagai and K. Asai, Development of Low-Density Wind Tunnel for Simulating Martian Atmospheric Flight, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.9, pp.21-27, 2011.04.
16. D. Numata, K. Ohtani, M. Anyoji, K. Takayama, M. Sun, Experimental study of hypervelocity impacts at low temperatures, Shock Waves, Vol.18, No.3, pp.169-183, 2008.07.
17. K. Kondo, H. Aono, T. Nonomura, M. Anyoji, A. Oyama, T. Liu, K. Fujii, M. Yamamoto, Analysis of Owl-like airfoil aerodynamics at low Reynolds number, Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 12, No. ists29, Tk_35-Tk_40, 2014.05.
18. D. Numata, K. Ohtani, M. Anyoji, K. Takayama, K. Togami, M. Sun, HVI tests on CFRP laminates at low temperature, International Journal of Impact Engineering, Vol.35, No.12, pp.1695-1701, 2008.08.
Presentations
1. M.Anyoji, D. Numata, H. Nagai, K. Asai , Experimental Studies on Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoils
, 2020 AIAA SciTech Forum and Exposition, 2020.01.
2. Masayuki ANYOJI, Hiroyuki KUDO, Daiki TAKAOKA, Keigo SHIMIZU, Takuji NAKAJIMA, Satoshi SEKIMOTO, Kozo FUJII , Flow Field Analysis around Ahmed Body using Global Luminescent Oil-Film Skin-Friction Meter, 50th Fluid Dynamics Conference of JSASS/36th Aerospace Numerical Simulation Symposium, 2018.06.
3. H. Aono, M. Anyoji, D. Hamada, S. Wakui, T. Tatsukawa, A Study on Development of Airfoil Shape Toward Low Reynolds-Number Dependence of Aerodynamics Under Low-Reynolds-Number-Flow Conditions, 2018 AIAA Scitech, 2018.01.
4. Akira Oyama, Hiroki Nagai, Hiroshi Tokutake, Koji Fujita, Anyoji Masayuki, Hiroyuki Toyota, Yu Miyazawa, Koichi Yonemoto, Masato Okamoto, Taku Nonomura, Masakazu Motoda, Shinsuke Takeuchi, Yukio Kamata, Masatsugu Otsuki, Keisuke Asai, Kozo Fujii, Flight System of Mars Airplane Balloon Experiment-1 (MABE-1), 31th International Symposium on Space Technology and Science, 2017.06.
5. Anyoji Masayuki, Masato Okamoto, Koji Fujita, Hiroki Nagai, Akira Oyama, Evaluation of Aerodynamic Characteristics on Mars Airplane Balloon Experiment-1 (MABE-1), 31th International Symposium on Space Technology and Science, 2017.06.
6. Anyoji Masayuki, Issei Tabaru, Toshiyuki Aoki, Reducing Jet Noise in Over-Expanded Nozzle Flow, Proceedings of 6th Asian Joint Workshop on Thermophysics and Fluid Science, 2016.09.
7. Hiroki Nagai, Anyoji Masayuki, Taku Nonomura, Akira Oyama, Masato Okamoto, Gaku Sasaki, Takaaki Matsumoto, Kouichi Yonemoto, Kasahiro Kanazaki, Shigeru Sunada, Koichi Yonezawa, Masaru Koike, Koji Fujita, Keisuke Asai, Kozo Fujii, Aerodynamic Challenges to Realize Mars Airplane, 30th International Symposium on Space Technology and Science, 2015.07.
8. K. Kondo, H. Aono, T. Nonomura, M. Anyoji, A. Oyama, T. Liu, K. Fujii, M. Yamamoto, Analysis of Owl-like airfoil aerodynamics at low Reynolds number, 29th International Symposium on Space Technology and Science, 2013.06.
9. M. Anyoji, D. Numata, H. Nagai, K. Asai, Evaluation of Supersonic Ejector Driving Performance under Low Pressure, 6th International Conference on Flow Dynamics, 2009.11.
10. M. Anyoji, M. Sun, Computer analysis of the schlieren optical setup, 27th International Congress on High-Speed Photography and Photonics, 2006.09.