Takayuki Nagata
Takayuki Nagata
Department of Aerospace Engineering, Tohoku University
確認したメール アドレス: aero.mech.tohoku.ac.jp - ホームページ
タイトル
引用先
引用先
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), 056101, 2016
542016
A simple immersed boundary method for compressible flow simulation around a stationary and moving sphere
Y Mizuno, S Takahashi, T Nonomura, T Nagata, K Fukuda
Mathematical problems in Engineering 2015, 2015
262015
Direct numerical simulation of flow around a heated/cooled isolated sphere up to a Reynolds number of 300 under subsonic to supersonic conditions
T Nagata, T Nonomura, S Takahashi, Y Mizuno, K Fukuda
International Journal of Heat and Mass Transfer 120, 284-299, 2018
182018
Experimental investigation on compressible flow over a circular cylinder at Reynolds number of between 1000 and 5000
T Nagata, A Noguchi, K Kusama, T Nonomura, A Komuro, A Ando, K Asai
Journal of Fluid Mechanics 893, 2020
112020
Experimental investigation of transonic and supersonic flow over a sphere for Reynolds numbers of 10 3–10 5 by free-flight tests with schlieren visualization
T Nagata, A Noguchi, T Nonomura, K Ohtani, K Asai
Shock Waves 30 (2), 139-151, 2020
102020
Determinant-based fast greedy sensor selection algorithm
Y Saito, T Nonomura, K Yamada, K Nakai, T Nagata, K Asai, Y Sasaki, ...
IEEE Access 9, 68535-68551, 2021
92021
Direct numerical simulation of subsonic, transonic and supersonic flow over an isolated sphere up to a Reynolds number of 1000
T Nagata, T Nonomura, S Takahashi, K Fukuda
Journal of Fluid Mechanics 904, 2020
92020
Direct numerical simulation of flow past a transversely rotating sphere up to a Reynolds number of 300 in compressible flow
T Nagata, T Nonomura, S Takahashi, Y Mizuno, K Fukuda
Journal of Fluid Mechanics 857, 878-906, 2018
82018
Direct numerical simulation of flow past a sphere at a Reynolds number between 500 and 1000 in compressible flows
T Nagata, T Nonomura, S Takahashi, Y Mizuno, K Fukuda
2018 AIAA Aerospace Sciences Meeting, 0381, 2018
82018
Effect of objective function on data-driven greedy sparse sensor optimization
K Nakai, K Yamada, T Nagata, Y Saito, T Nonomura
IEEE Access 9, 46731-46743, 2021
62021
Optimum pressure range evaluation toward aerodynamic measurements using PSP in low-pressure conditions
T Nagata, M Kasai, T Okudera, H Sato, T Nonomura, K Asai
Measurement Science and Technology 31 (8), 085303, 2020
42020
Numerical simulation on solid–liquid multiphase flow including complex-shaped objects with collision and adhesion effects using immersed boundary method
M Hosaka, T Nagata, S Takahashi, K Fukuda
Multiphase Flow Theory Appl 6 (1), 162-175, 2018
32018
Data-driven sparse sensor placement based on A-optimal design of experiment with ADMM
T Nagata, T Nonomura, K Nakai, K Yamada, Y Saito, S Ono
arXiv preprint arXiv:2010.09329, 2020
22020
Direct Numerical Simulation of Shock Waves Passed by Multiple Particles by Using Immersed Boundary Method
Y Mizuno, S Takahashi, T Nonomura, T Nagata, K Fukuda
54th AIAA Aerospace Sciences Meeting, 0618, 2016
22016
Determinant-Based Fast Greedy Sensor Selection Algorithm.(2019)
Y Saito, T Nonomura, K Yamada, K Asai, Y Sasaki, D Tsubakino
arXiv preprint arXiv:1911.08757, 0
2
Supersonic and Hypersonic Drag Coefficients for a Sphere
E Loth, J Tyler Daspit, M Jeong, T Nagata, T Nonomura
AIAA Journal 59 (8), 3261-3274, 2021
12021
Data-driven sparse sensor selection based on A-optimal design of experiment with ADMM
T Nagata, T Nonomura, K Nakai, K Yamada, Y Saito, S Ono
IEEE Sensors Journal, 2021
12021
Investigation of Mach number effects on flow over a flat plate at Reynolds number of 1.0× 104 by schlieren visualization
K Kusama, T Nagata, M Anyoji, T Nonomura, K Asai
Fluid Dynamics Research 53 (1), 015513, 2021
12021
Frequency Response of Pressure-Sensitive Paints under Low-Pressure Conditions
M Kasai, D Sasaki, T Nagata, T Nonomura, K Asai
Sensors 21 (9), 3187, 2021
12021
Effect of Oxygen Mole Fraction on Static Properties of Pressure-Sensitive Paint
T Okudera, T Nagata, M Kasai, Y Saito, T Nonomura, K Asai
Sensors 21 (4), 1062, 2021
12021
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