Suitable time step for Ffowcs Williams and Hawkings
Hi all,
I have a question on the selection of the proper time step when performing an aeroacoustic calculation with the Ffowcs Williams and Hawkings (FW-H) model. The case is a low-speed propeller (5 blades, maximum Mach number is 0.2) with air at 20 degrees. Additional details of my setup are:
I have some noise experimental data at disposal in the range [10-10000] Hz, and the main contribution to the sound power level is up to 5000 Hz: hence, for the purpose of this investigation (and to avoid the cell count to skyrocket), I have generated a mesh with a cell size corresponding to 15 points per wavelength at 5000 Hz. Considering the maximum frequency of 10000 Hz and the Nyquist theorem, I set a time step of 0.00005 s (i.e. the inverse of the sampling frequency). This time step guarantees the physical CFL to be < 1, and I am running the case for enough rotations in order to have a frequency resolution of 2-3 Hz. Additionally, the IDDES blending function contour results to be correct and the mesh has a y+ < 1. However, it is not fully clear to me if the approach I have followed to select the time step is correct to have an accurate aeroacoustic simulation or if I should further refine it ? I have checked the STAR-CCM+ theory and tutorial for the FW-H model (cylinder crossflow): they describe different ways of selecting the time step for the FW-H model (some seem somehow related to the use of the perturbed convective wave equation, which is not my case), but I could not find an answer that clarifies my question/doubt. Can you please provide a feedback ? Thanks ! |
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