Taku Nonomura
Taku Nonomura
Department of Aerospace Engineering, Graduate School of Engineering, Nagoya University
Zweryfikowany adres z mae.nagoya-u.ac.jp - Strona główna
Cytowane przez
Cytowane przez
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
Freestream and vortex preservation properties of high-order WENO and WCNS on curvilinear grids
T Nonomura, N Iizuka, K Fujii
Computers & Fluids 39 (2), 197-214, 2010
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
Mechanisms for laminar separated-flow control using dielectric-barrier-discharge plasma actuator at low Reynolds number
M Sato, T Nonomura, K Okada, K Asada, H Aono, A Yakeno, Y Abe, ...
Physics of Fluids 27 (11), 2015
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
Robust Explicit Formulation of Weighted Compact Nonlinear Scheme
T Nonomura, K Fujii
Computers & Fluids, 2013
Effects of difference scheme type in high-order weighted compact nonlinear schemes
T Nonomura, K Fujii
Journal of Computational Physics 228 (10), 3533-3539, 2009
ADI-SGS scheme on ideal magnetohydrodynamics
H Nishida, T Nonomura
Journal of Computational Physics 228 (9), 3182-3188, 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
Investigation on subsonic to supersonic flow around a sphere at low Reynolds number of between 50 and 300 by direct numerical simulation
T Nagata, T Nonomura, S Takahashi, Y Mizuno, K Fukuda
Physics of Fluids 28 (5), 2016
Multifactorial effects of operating conditions of dielectric-barrier-discharge plasma actuator on laminar-separated-flow control
M Sato, H Aono, A Yakeno, T Nonomura, K Fujii, K Okada, K Asada
AIAA journal 53 (9), 2544-2559, 2015
Burst-mode frequency effects of dielectric barrier discharge plasma actuator for separation control
S Sekimoto, T Nonomura, K Fujii
AIAA journal 55 (4), 1385-1392, 2017
Aeroacoustic waves generated from a supersonic jet impinging on an inclined flat plate
T Nonomura, Y Goto, K Fujii
International Journal of Aeroacoustics 10 (4), 401-425, 2011
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
Geometric interpretations and spatial symmetry property of metrics in the conservative form for high-order finite-difference schemes on moving and deforming grids
Y Abe, T Nonomura, N Iizuka, K Fujii
Journal of Computational Physics 260, 163-203, 2014
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
A new technique for freestream preservation of finite-difference WENO on curvilinear grid
T Nonomura, D Terakado, Y Abe, K Fujii
Computers & Fluids 107, 242-255, 2015
A numerical scheme based on an immersed boundary method for compressible turbulent flows with shocks: application to two‐dimensional flows around cylinders
S Takahashi, T Nonomura, K Fukuda
Journal of Applied Mathematics 2014 (1), 252478, 2014
Numerical (error) issues on compressible multicomponent flows using a high-order differencing scheme: weighted compact nonlinear scheme
T Nonomura, S Morizawa, H Terashima, S Obayashi, K Fujii
Journal of Computational Physics 231 (8), 3181-3210, 2012
Unified mechanisms for separation control around airfoil using plasma actuator with burst actuation over Reynolds number range of 103–106
M Sato, K Okada, K Asada, H Aono, T Nonomura, K Fujii
Physics of Fluids 32 (2), 2020
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