| 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. |
