Near-wall modification of Spalart–Allmaras turbulence model for immersed boundary method Y Tamaki, M Harada, T Imamura AIAA journal 55 (9), 3027-3039, 2017 | 100 | 2017 |
Designing of slat cove filler as a noise reduction device for leading-edge slat T Imamura, H Ura, Y Yokokawa, S Enomoto, K Yamamoto, T Hirai 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference …, 2007 | 98 | 2007 |
Acceleration of steady-state lattice Boltzmann simulations on non-uniform mesh using local time step method T Imamura, K Suzuki, T Nakamura, M Yoshida Journal of Computational Physics 202 (2), 645-663, 2005 | 96 | 2005 |
Three-dimensional unsteady flow computations around a conventional slat of high-lift devices T Imamura, S Enomoto, Y Yokokawa, K Yamamoto AIAA journal 46 (5), 1045-1053, 2008 | 79 | 2008 |
A far-field noise and near-field unsteadiness of a simplified high-lift-configuration model (slat) T Imamura, H Ura, Y Yokokawa, K Yamamoto 47th AIAA aerospace sciences meeting including the new horizons forum and …, 2009 | 62 | 2009 |
Turbulent flow simulations of the common research model using immersed boundary method Y Tamaki, T Imamura AIAA journal 56 (6), 2271-2282, 2018 | 50 | 2018 |
Experimental study on noise generation of a two-wheel main landing gear Y Yokokawa, T Imamura, H Ura, H Uchida, K Yamamoto, H Kobayashi 16th AIAA/CEAS Aeroacoustics Conference, 3973, 2010 | 48 | 2010 |
Investigation of airframe noise from high lift configuration model H Ura, Y Yokokawa, T Imamura, T Ito, K Yamamoto 46th AIAA Aerospace Sciences Meeting and Exhibit, 19, 2008 | 45 | 2008 |
Flow simulation around an airfoil by lattice Boltzmann method on generalized coordinates T Imamura, K Suzuki, T Nakamura, M Yoshida AIAA journal 43 (9), 1968-1973, 2005 | 45 | 2005 |
Aerodynamic and aeroacoustic simulations of a two-wheel landing gear T Imamura, T Hirai, K Amemiya, Y Yokokawa, S Enomoto, K Yamamoto Procedia Engineering 6, 293-302, 2010 | 36 | 2010 |
Studies on Airframe Noise Generation at High-lift Devices in Relation to Aerodynamic Performances Y Yokokawa, T Imamura, H Ura, H Uchida, T Ito, K Yamamoto 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference …, 2008 | 29 | 2008 |
Simple and robust cut-cell method for high-Reynolds-number-flow simulation on Cartesian grids M Harada, Y Tamaki, Y Takahashi, T Imamura AIAA journal 55 (8), 2833-2841, 2017 | 25 | 2017 |
Numerical investigation on change of airframe noise by flap side-edge shape M Murayama, Y Yokokawa, K Yamamoto, H Ura, T Imamura, T Hirai 19th AIAA/CEAS Aeroacoustics Conference, 2067, 2013 | 24 | 2013 |
Simulation of the broadband noise from a slat using zonal les/rans hybrid method T Imamura, S Enomoto, Y Yokokawa, K Yamamoto 45th AIAA Aerospace Sciences Meeting and Exhibit, 226, 2007 | 24 | 2007 |
Experimental and numerical studies on flow behind a circular cylinder based on POD and DMD M Sakai, Y Sunada, T Imamura, K Rinoie Transactions of the Japan Society for Aeronautical and Space Sciences 58 (2 …, 2015 | 21 | 2015 |
Numerical and Experimental Research of Low-Noise Slat Using Simplified High-lift Model T Imamura, H Ura, Y Yokokawa, T Hirai, K Yamamoto 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference …, 2008 | 21 | 2008 |
Flow simulation around an airfoil using lattice Boltzmann method on generalized coordinates T Imamura, K Suzuki, T Nakamura, M Yoshida 42nd AIAA aerospace sciences meeting and exhibit, 244, 2004 | 20 | 2004 |
A Far-field Noise and Near-field Unsteadiness of a Simplified High-lift-configuration Model (Flap-edge) Y Yokokawa, T Imamura, H Ura, K Yamamoto 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and …, 2009 | 19 | 2009 |
Unsteady flow simulation around cylinder under airfoil using cartesian-based flow solver T Imamura, Y Takahashi 21st AIAA Computational Fluid Dynamics Conference, 2857, 2013 | 17 | 2013 |
3D Unsteady Flow Computations in a Slat Cove Using Large Eddy Simulation T Imamura, S Enomoto, K Yamamoto 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference …, 2006 | 17 | 2006 |