Kyushu University Academic Staff Educational and Research Activities Database
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Anyoji Masayuki Last modified date:2017.12.01

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


Graduate School
Undergraduate School


E-Mail
Phone
092-583-7590
Academic Degree
Ph.D in Engineering
Field of Specialization
Experimental Gas Dynamics, Fluid Measurement
Research
Research Interests
  • Development of high performance wing at low Reynolds numbers
    keyword : low Reynolds number, mars airplane, high performance wing
    2015.04~2017.07.
  • Shock wave oscillation in two dimensional C-D nozzle
    keyword : supersonic, shock wave, jet flow, acoustic
    2014.10.
  • Development of Surface Skin Friction Measurement Technique
    keyword : Skin friction, Non-contact, Luminescent oil-film skin-friction meter
    2014.04.
  • Fluid Dynamics of Low-Reynolds-Number Airfoils
    keyword : Low Reynolds number, airfoil, aerodynamics, separation bubble
    2011.04~2014.03.
  • 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. 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.
2. 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, 2017.09.
3. 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, 27, 2, 2015.02.
4. 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, Vol. 18, Isuue 2, 2014.10.
5. Masayuki Anyoji, Daiju Numata, Hiroki Nagai, Keisuke Asai, Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows, AIAA Journal, Vol. 53, Issue 6, 2015.05.
6. 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, Vol. 51, No. 6, 2014.12.
7. 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, Vol.9, No.5, No. 14-00176, 2014.11.
8. 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, 2014.01.
9. 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, 2011.04.
10. D. Numata, K. Ohtani, M. Anyoji, K. Takayama, M. Sun, Experimental study of hypervelocity impacts at low temperatures, Shock Waves, Vol.18, No.3, 2008.07.
11. 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, 2014.05.
12. 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, 2008.08.
Presentations
1. 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, 2017.06.09.
2. 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, 2017.06.09.
3. 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, 2016.09.22.
4. 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, 2015.07.09.
5. 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, 2013.06.02.
6. M. Anyoji, D. Numata, H. Nagai, K. Asai, Evaluation of Supersonic Ejector Driving Performance under Low Pressure, 6th International Conference on Flow Dynamics, 2009.11.04.
7. M. Anyoji, M. Sun, Computer analysis of the schlieren optical setup, 27th International Congress on High-Speed Photography and Photonics, 2006.09.17.