Akira Oyama
Zitiert von
Zitiert von
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
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
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
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
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
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
Multiobjective optimization of rocket engine pumps using evolutionary algorithm
A Oyama, MS Liou
Journal of Propulsion and Power 18 (3), 528-535, 2002
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
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
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
Multidisciplinary optimization of transonic wing design based on evolutionary algorithms coupled with CFD solver
A Oyama
CD-ROM Proceeding of the European Congress on Computational Methods in …, 2000
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
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
Wing design using evolutionary algorithms
A Oyama
Department of Aeronautics and Space Engineering of Tohoku University, 2000
A study on airfoil design for future Mars airplane
A Oyama, K Fujii
44th AIAA Aerospace Sciences Meeting and Exhibit, 1484, 2006
Crosstalk of prolyl isomerases, Pin1/Ess1, and cyclophilin A
F Fujimori, W Gunji, J Kikuchi, T Mogi, Y Ohashi, T Makino, A Oyama, ...
Biochemical and biophysical research communications 289 (1), 181-190, 2001
Benchmarking multi-and many-objective evolutionary algorithms under two optimization scenarios
R Tanabe, H Ishibuchi, A Oyama
IEEE Access 5, 19597-19619, 2017
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
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
Aerodynamic multiobjective design exploration of a flapping airfoil using a navier-stokes solver
A Oyama, Y Okabe, K Shimoyama, K Fujii
Journal of Aerospace Computing, Information, and Communication 6 (3), 256-270, 2009
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