Abstract:A study has been made of the flow and heat transfer to a circular cylinder from an isothermal impinging air jet. Numerical solutions of the governing conservation equations have been obtained utilizing a non-orthogonal curvilinear coordinate grid. The study focused on low Reynolds numbers (based on nozzle average exit velocity and cylinder diameter) in the range of 132-1315 and H/W = 2, 4, 6 and 8 which corresponds to the ratio of distance between the nozzle and cylinder to nozzle width. The flow is stable and… Show more
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