Active control of compressible supersonic wall-bounded flow using direct numerical simulations with spanwise velocity modulation at the walls using PyFR
Prof. Dr. Holger Foysi
Summary (AI generated)
The discussion began by mentioning that research on reduced rubble and chilly growth was done by Bradshaw in 1977, with increasing convective Mach number. The flow stabilization in the supersonic regime was also studied by Soccer, who had worked together with the speaker in San Diego. Turbulent production was found to decrease along with pressure fluctuations, which is an important quantity in compressible flow. Numerous authors such as Freeman, Sarkar, Fraud, and Pantano have researched this topic.
In supersonic channel flows, there is an increase in anisotropy regarding turbulent stresses, where the stream of stress increases, while the other stresses decrease. The speaker explained that one of the reasons for this is the strong decrease in the pressure strain coalition. The pressure gradient at each point is determined by the momentum transfer of the largest rounding, which is called the vortex region. The speaker explained that this region could be determined using two-point correlations and that it affects pressure fluctuations. The speaker also mentioned that this effective density mapping could be used to show compressive results under incompressible ones.
The pressure strain coalition is an important quantity not only in fresh air flows but also in wall-bounded flow shows. The speaker also discussed how this coalition relates to other types of flows, such as isotropic and psychotropic turbulence. In the speaker's PhD research, gradients with most were examined, and different key quantities transporting patients of the invariants to see how that developed.