TY  - THES
U1  - Master Thesis
A1  - Sokolov, Sebastian
T1  - Analysis of Non-Reflecting Boundary Conditions for Direct Aeroacoustic Simulation with the Lattice Boltzmann Method
N2  - The Lattice Boltzmann Method is a useful tool to calculate fluid flow and acoustic effects at the same time. Although the acoustic perturbation is much smaller than normal pressure differences in fluid flow, this direct calculation is a great advantage of the Lattice Boltzmann Method (LBM). But each border used in calculation produces a multitude of reflections with the acoustic waves, which lead to an unusable result. Therefore, it is worked on different absorbing techniques.
In this thesis three absorbing layer techniques are described, explained and reviewed with different simulations. The absorbing layers are implemented in a basic LBM code in C++, and with this umpteen simulations within a box were performed to compare the different absorbing layers. The Doppler effect and a cylinder flow are also examined to compare the damping efficiencies.
The three studied absorbing techniques are the sponge layer, the perfectly matched layer and a force based Term II absorbing layer. The sponge layer is easy to implement but gives worse results than a calculation without any absorbing layer. The perfectly matched layer and a force based absorbing term provide very good results but the perfectly matched layer has problems with instability. The force based absorbing layer represents the best compromise between the additional computation time due the absorbing layer and the achieved damping efficiency.
KW  - Lattice Boltzmann Method
KW  - Non-Reflecting Boundary Conditions
KW  - Direct Aeroacoustic Simulation
Y2  - 2021
SP  - VI, 80
S1  - VI, 80
CY  - Offenburg
ER  -