Numerical Simulation of Aeroacoustic Noise at Low Mach Number Flows by Using the Finite Difference Lattice Boltzmann Method |
Eun-Ra Kim
(전북대학교 공업기술연구센터)
Jeong-Hwan Kim (한국조선기자재연구) Ho-Keun Kang (경상대학교 기계항공공학부ㆍ해양산업연구소) |
1 |
On the Finite Difference-based Lattice Boltzmann Method in Curvilinear Coordinates
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ScienceOn |
2 |
An Acoustic/Viscous Splitting Technique for Computational Aeroacoustics
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3 |
Aeroacoustic Computation of Cylinder Wake Flow
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ScienceOn |
4 |
Computation of Vortex Shedding and Radiated Sound for a Cirular Cylinder: Subcritical to Transonic Reynolds Numbers
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ScienceOn |
5 |
Comment on the Aeroacoustic Formulation of Hardin and pope
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ScienceOn |
6 |
Computational Aeroacoustic Simulation using the Expansion about Incompressible Flow Approach
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ScienceOn |
7 |
Sound Generation in a Mixing Layer
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8 |
Sound Generation by a two-dimensional Circular Cylinder in a Uniform Flow
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9 |
Lattice Boltzmann Method for Fluid Flows
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ScienceOn |
10 |
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11 |
Physical Symmetry and Lattice Symmetry in the Lattice Boltzmann Method
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12 |
Boundary Conditions for Direct Simulation of Compressible Viscous Flows
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13 |
Lattice Boltzmann Simulations of Liquid-gas and Binary Fluid Systems
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14 |
Numerical Simulation of Shock Wave Propagation Using the Finite Diference Lattice Boltzmann Method
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15 |
Numerical Simulation of Aerodynamic Sound by the Finite Diference Lattice Boltzmann Method
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16 |
Lattice Boltzmann Scheme for Simulating Two-Phase Flows
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17 |
A Model for Collision Processes in Gases. I. Small Amplitude Prosesses in Charged and Neutral One-component Systems
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