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Anyoji Masayuki Last modified date：2023.01.27

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


Graduate School
Department of Energy and Environmental Engineering
Interdisciplinary Graduate School of Engineering Sciences
Undergraduate School
Department of Energy Science and Engineering
School of Engineering


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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
 Show All Papers >>
1. T. Yamaguchi, M. Anyoji, Numerical Study on Low-Reynolds Compressible Flows Around Mars Helicopter Rotor Blade Airfoil, Journal of Flow Control, Measurement & Visualization, accepted for publication, 2023.01.
2. S. Sekimoto, K. Fujii, M. Anyoji, Y, Miyakawa, S. Ito, S. Shimomura, H. Nishida, T. Nonomura, T. Matsuno, Flow Control around a NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of Reynolds Number, Actuators, https://doi.org/10.3390/act12010043, Vol. 12, Issue 1, 43,, 2023.01.
3. T. H. Tran, M. Hijikuro, M. Anyoji, T. Uchida, T. Nakashima, and K. Shimizu, Effect of a short, bio-mimetic control device on aerodynamic drag of Ahmed body, Journal of Fluids Engineering, https://doi.org/10.1115/1.4056341, Vol. 145, Issue 3, 03106, 2023.03.
4. T. H. Tran, M. Hijikuro, M. Anyoji, T. Uchida, T. Nakashima, and K. Shimizu, Deflector effect on flow behavior and drag of an Ahmed body under crosswind conditions, Journal of Wind Engineering & Industrial Aerodynamics, https://doi.org/10.1016/j.jweia.2022.105238, Vol. 231, 105238, 2022.11.
5. Hiroki Mukohara, Masayuki Anyoji, Computational analysis of compressibility effect on flow field and aerodynamics at low Reynolds numbers, Physics of Fluids, https://doi.org/10.1063/5.0079186, Vol. 34, Issue 5, No. 056109, 2022.05.
6. The Hung Tran , Masayuki Anyoji, Takuji Nakashima, Keigo Shimizu, Anh Dinh Le, Experimental study of the skin-friction topology around the Ahmed body in cross-wind conditions, Journal of Fluids Engineering, https://doi.org/10.1115/1.4052418, Vol. 144, No. 3, 031209, 2022.03.
7. Masayuki Anyoji, Fujio Akagi, Yu Matsuda, Yasuhiro Egami, Taro Handa, Mechanism of supersonic mixing enhancement by a wall-mounted three-dimensional cavity, Acta Astronautica, https://doi.org/10.1016/j.actaastro.2021.08.019, Vol. 188, pp. 491-504, 2021.11.
8. Shuichi Hiramatsu, Masayuki Anyoji, Koji Fujita, Hiroki Nagai, Akira Oyama, Hiroyuki Kato, Aeroelastic deformation measurement of Martian airplane for high-altitude flight experiment using stereophotogrammetry, Engineering Research Express, https://doi.org/10.1088/2631-8695/abe920, Vol.3, No.1, 015035, 2021.03.
9. Kensuke Kusama, Takayuki Nagata, Masayuki Anyoji, Taku Nonomura and Keisuke Asai, Investigation of mach number effects on flow over a flat plate at Reynolds number of 1.0 × 104 by Schlieren visualization, Fluid Dynamics Research, https://doi.org/10.1088/1873-7005/abe04c, Vol.53, No.1, 015513, 2021.02.
10. T. Sato, S. Sakuma, M. Hijikuro, S. Maeda, M. Anyoji, Y. Yamanishi, Design of electrohydrodynamic devices with consideration of electrostatic energy, Cyborg and Bionic Systems, https://doi.org/10.34133/2021/5158282, Vol.2021, Article ID 5158282, 2021.01.
11. Masayuki ANYOJI, Daiju NUMATA, Hiroki NAGAI, Keisuke ASAI, Supersonic Ejector-Driving System Under Low Pressure : A Performance Evaluation, Transaction of the Japan Society for Aeronautical and Space Sciences, https://doi.org/10.2322/tjsass.64.156, Vol. 64, No. 3, pp. 156-164, 2021.05.
12. K. Kajiwara, M. Anyoji, Turbulence Intensity Effects on a Leading-Edge Separation Bubble of Flat Plate Wing at Low-Reynolds Numbers, Journal of Flow Control, Measurement & Visualization, https://doi.org/10.4236/jfcmv.2020.84012, Vol. 8, No. 4, 188-207, 2020.10.
13. M. Hijikuro,M. Anyoji, Application of Optical Flow Analysis to Shadowgraph Images of Impinging Jet, Journal of Flow Control, Measurement & Visualization, 10.4236/jfcmv.2020.84011 , Vol. 8, No. 4, 173-187, 2020.09.
14. 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, https://doi.org/10.2322/tjsass.63.8, Vol. 63, No. 1, 8-17, 2020.01.
15. 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.
16. 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.
17. 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.
18. 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.
19. 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.
20. 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.
21. 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.
22. 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..
23. 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.
24. 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.
25. 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.
26. 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.
27. 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.
28. 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.
29. 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
 Show All Presentations >>
1. T. H. Tran, M. Hijikuro, M. Anyoji, T. Uchida, T. Nakashima, and K. Shimizu, Flow Topology on the Ahmed Body with a Deflector by a Sub-grid Global Skin-Friction Measurement Method, Nineteenth International Conference on Flow Dynamics, 2022.11.
2. T. Yamaguchi and M. Anyoji, Numerical Study on Low-Reynolds Compressible Flows around the Airfoil of the Rotor Blade for Mars Helicopter, The 2022 Asia-Pacific International Symposium on Aerospace Technology , 2022.10.
3. Masato Hijikuro, Masayuki Anyoji, Extension of Applicable Flow Velocity Range for High-Speed Impinging Jet by Optical Flow Analysis, 33rd International Symposium on Space Technology and Science, 2022.02.
4. 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.
5. 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.
6. 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.
7. 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.
8. 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.
9. 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.
10. 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.
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, 29th International Symposium on Space Technology and Science, 2013.06.
12. 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.
13. M. Anyoji, M. Sun, Computer analysis of the schlieren optical setup, 27th International Congress on High-Speed Photography and Photonics, 2006.09.


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