The effect of synthetic jets on heat fluxes in a transitional channel with flow separation

Current Review on Numerical Simulation of Synthetic Jet (SJ) Cooling

“…Researchers frequently utilise the Semi-Implicit Method for Pressure Linked Equations (SIMPLE) technique to model incompressible flow because it works well for unsteady flow with tiny time steps. [12] 1, 4, 100, 200, 400 300,1200 Benayad et al, [14] 10,000 5-20 Liu et al, [18] 100-200 -Li et al, [22] 10,20,50 10,000 -20,000 Zhang et al, [29] 0 [9] Cylindrical Circular Kane et al, [18] Cylindrical Circular Guo et al, [21] Cylindrical Circular Kumar et al, [27] Cylindrical Slot Zhu et al, [33] Cylindrical Slot Qiu et al, [34] Cylindrical Circular Jacob et al, [40] Cylindrical Circular Ahmad and Qayoum [51] Cylindrical Circular…”

“…Belova et al, [51] has carried out computational studies of the impact of SJ on the flow in the model transition channel. Due to the huge diffuser expansion angle, a detachment flow forms in the channel, which is physically induced by a positive pressure gradient on the wall; Heat flux into the wall increases in the zone of separated flow; the highest heat flux is seen at the attachment point of the separation flow.…”