Article ID Journal Published Year Pages File Type
7052259 Experimental Thermal and Fluid Science 2015 11 Pages PDF
Abstract
For low swirl flows, the coefficient of pressure (Cp) shows a non-swirl like behaviour with maxima at the stagnation point. For medium-to-high swirls, maximum Cp shifts radially outward from the stagnation point and becomes relatively flat with increasing S. The stagnation pressure reduces nonlinearly with increasing swirl intensity and follows a quadratic relationship for a given Re. For any S, the pressure distribution is found to be independent of Re for low swirl numbers (up to S = 0.3), but it varies up to r/D = 2 for larger swirl numbers. A negative Cp (flow separation) occurs near the stagnation region for H = 1D, however, vanishes at larger H. For very high swirl number (S = 1.05) and at H = 1D, three different regions are recognised on the impingement surface from the stagnation point: a rotating, reversed inward flow at r/D ⩽ 0.5, a transition and less stable region at 0.5 < r/D ⩽ 0.75 and an outward flow with stronger tangential component at r/D ⩾ 1.0. These surface pressure results may significantly affect the heat transfer characteristics as well as wall shear stresses for future impinging jet studies.
Related Topics
Physical Sciences and Engineering Chemical Engineering Fluid Flow and Transfer Processes
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