| Transonic axial-flow blade optimization: Evolutionary algorithms/three-dimensional Navier-Stokes solver A Oyama, MS Liou, S Obayashi Journal of Propulsion and Power 20 (4), 612-619, 2004 | 307 | 2004 |
| Real-coded adaptive range genetic algorithm applied to transonic wing optimization A Oyama, S Obayashi, T Nakamura Applied Soft Computing 1 (3), 179-187, 2001 | 135 | 2001 |
| 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 | 132 | 2014 |
| Large-eddy simulation of low-Reynolds-number flow over thick and thin NACA airfoils R Kojima, T Nonomura, A Oyama, K Fujii Journal of Aircraft 50 (1), 187-196, 2013 | 119 | 2013 |
| Airfoil flow experiment on the duty cycle of DBD plasma actuator K Asada, Y Ninomiya, K Fujii, A Oyama 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and …, 2009 | 114 | 2009 |
| Data mining of Pareto-optimal transonic airfoil shapes using proper orthogonal decomposition A Oyama, T Nonomura, K Fujii Journal of Aircraft 47 (5), 1756-1762, 2010 | 107 | 2010 |
| Benchmarking multi-and many-objective evolutionary algorithms under two optimization scenarios R Tanabe, H Ishibuchi, A Oyama IEEE Access 5, 19597-19619, 2017 | 90 | 2017 |
| Lactate increases myotube diameter via activation of MEK/ERK pathway in C2C12 cells Y Ohno, A Oyama, H Kaneko, T Egawa, S Yokoyama, T Sugiura, Y Ohira, ... Acta physiologica 223 (2), e13042, 2018 | 88 | 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 | 80 | 2015 |
| Progress in design optimization using evolutionary algorithms for aerodynamic problems Y Lian, A Oyama, MS Liou Progress in Aerospace Sciences 46 (5-6), 199-223, 2010 | 80 | 2010 |
| Multidisciplinary design optimization and data mining for transonic regional-jet wing K Chiba, A Oyama, S Obayashi, K Nakahashi, H Morino Journal of Aircraft 44 (4), 1100-1112, 2007 | 75 | 2007 |
| Multiobjective optimization of rocket engine pumps using evolutionary algorithm A Oyama, MS Liou Journal of Propulsion and Power 18 (3), 528-535, 2002 | 75 | 2002 |
| New constraint-handling method for multi-objective and multi-constraint evolutionary optimization A Oyama, K Shimoyama, K Fujii Transactions of the Japan Society for Aeronautical and Space Sciences 50 …, 2007 | 70 | 2007 |
| A study on airfoil design for future Mars airplane A Oyama, K Fujii 44th AIAA Aerospace Sciences Meeting and Exhibit, 1484, 2006 | 68 | 2006 |
| A note on constrained multi-objective optimization benchmark problems R Tanabe, A Oyama 2017 IEEE Congress on Evolutionary Computation (CEC), 1127-1134, 2017 | 62 | 2017 |
| Finding tradeoffs by using multiobjective optimization algorithms S Obayashi, D Sasaki, A Oyama Transactions of the Japan Society for Aeronautical and Space Sciences 47 …, 2004 | 54 | 2004 |
| Closed-loop flow separation control using the deep Q network over airfoil S Shimomura, S Sekimoto, A Oyama, K Fujii, H Nishida AIAA Journal 58 (10), 4260-4270, 2020 | 53 | 2020 |
| Multidisciplinary and multi-objective design exploration methodology for conceptual design of a hybrid rocket Y Kosugi, A Oyama, K Fujii, M Kanazaki Infotech@ Aerospace 2011, 1634, 2011 | 53 | 2011 |
| Multiobjective optimization of a multi-stage compressor using evolutionary algorithm A Oyama, MS Liou 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3535, 2002 | 53 | 2002 |
| A new efficient and useful robust optimization approach-design for multi-objective six sigma K Shimoyama, A Oyama, K Fujii 2005 IEEE Congress on Evolutionary Computation 1, 950-957, 2005 | 52 | 2005 |
