| Pressure and temperature sensitive paints T Liu, JP Sullivan, K Asai, C Klein, Y Egami Springer, 2005 | 1170 | 2005 |
| A review of pressure-sensitive paint for high-speed and unsteady aerodynamics JW Gregory, K Asai, M Kameda, T Liu, JP Sullivan Proceedings of the institution of mechanical engineers, part G: journal of …, 2008 | 444 | 2008 |
| A review of Backward-Facing Step (BFS) flow mechanisms, heat transfer and control L Chen, K Asai, T Nonomura, G Xi, T Liu Thermal Science and Engineering Progress 6, 194-216, 2018 | 209 | 2018 |
| Adsorptive pressure-sensitive coatings on porous anodized aluminium M Kameda, N Tezuka, T Hangai, K Asai, K Nakakita, Y Amao Measurement Science and Technology 15 (3), 489, 2004 | 123 | 2004 |
| Computational and experimental analysis of a high-performance airfoil under low-Reynolds-number flow condition M Anyoji, T Nonomura, H Aono, A Oyama, K Fujii, H Nagai, K Asai Journal of Aircraft 51 (6), 1864-1872, 2014 | 120 | 2014 |
| Image measurements of unsteady pressure fluctuation by a pressure-sensitive coating on porous anodized aluminium M Kameda, T Tabei, K Nakakita, H Sakaue, K Asai Measurement Science and Technology 16 (12), 2517, 2005 | 105 | 2005 |
| Novel pressure-sensitive paint for cryogenic and unsteady wind-tunnel testing K Asai, Y Amao, Y Iijima, I Okura, H Nishide Journal of thermophysics and heat transfer 16 (1), 109-115, 2002 | 101 | 2002 |
| Surface pressure measurement in a cryogenic wind tunnel by using luminescent coating K Asai, H Kanda, CT Cunningham, R Erausquin, JP Sullivan ICIASF'97 Record. International Congress on Instrumentation in Aerospace …, 1997 | 97 | 1997 |
| Nonlinear lift on a triangular airfoil in low-Reynolds-number compressible flow PM Munday, K Taira, T Suwa, D Numata, K Asai Journal of Aircraft 52 (3), 924-931, 2015 | 89 | 2015 |
| Transition detection by temperature sensitive paint at cryogenic temperatures in the European Transonic Wind tunnel (ETW) U Fey, RH Engler, Y Egami, Y Iijima, K Asai, U Jansen, J Quest 20th International Congress on Instrumentation in Aerospace Simulation …, 2003 | 87 | 2003 |
| Platinum porphyrin embedded in poly (1-trimethylsilyl-1-propyne) film as an optical sensor for trace analysis of oxygen Y Amao, K Asai, I Okura, H Shinohara, H Nishide Analyst 125 (11), 1911-1914, 2000 | 82 | 2000 |
| Experimental analysis of transonic buffet on a 3D swept wing using fast-response pressure-sensitive paint Y Sugioka, S Koike, K Nakakita, D Numata, T Nonomura, K Asai Experiments in Fluids 59, 1-20, 2018 | 80 | 2018 |
| Mechanisms of surface pressure distribution within a laminar separation bubble at different Reynolds numbers D Lee, S Kawai, T Nonomura, M Anyoji, H Aono, A Oyama, K Asai, K Fujii Physics of Fluids 27 (2), 2015 | 74 | 2015 |
| Effects of Mach number and specific heat ratio on low-Reynolds-number airfoil flows M Anyoji, D Numata, H Nagai, K Asai AIAA journal 53 (6), 1640-1654, 2015 | 73 | 2015 |
| Oxygen sensing based on lifetime of photoexcited triplet state of platinum porphyrin–polystyrene film using time‐resolved spectroscopy Y Amao, K Asai, I Okura Journal of Porphyrins and Phthalocyanines 4 (3), 292-299, 2000 | 73 | 2000 |
| Effect of temperature-sensitive-paint thickness on global heat transfer measurement in hypersonic flow H Nagai, S Ohmi, K Asai, K Nakakita Journal of Thermophysics and Heat Transfer 22 (3), 373-381, 2008 | 71 | 2008 |
| Novel optical oxygen sensing material: platinum porphyrin‐fluoropolymer film Y Amao, K Asai, T Miyashita, I Okura Polymers for Advanced Technologies 11 (8‐12), 705-709, 2000 | 71 | 2000 |
| Application of pressure-sensitive paints to low-pressure range T Niimi, M Yoshida, M Kondo, Y Oshima, H Mori, Y Egami, K Asai, ... Journal of thermophysics and heat transfer 19 (1), 9-16, 2005 | 66 | 2005 |
| Boundary-layer transition detection in a cryogenic wind tunnel using luminescent paint K Asai, H Kanda, T Kunimasu, T Liu, JP Sullivan Journal of Aircraft 34 (1), 34-42, 1997 | 65 | 1997 |
| Anodized aluminum pressure sensitive paint in a cryogenic wind tunnel H Sakaue ISA Proceedings of the 45th International Instrum. Sym., 1999, 345-354, 1999 | 63 | 1999 |
Taku NonomuraDepartment of Aerospace Engineering, Graduate School of Engineering, Nagoya University確認したメール アドレス: mae.nagoya-u.ac.jp
