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首页> 外文期刊>International Journal of Heat and Mass Transfer >Heat transfer characteristics of swirling and non-swirling impinging turbulent jets
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Heat transfer characteristics of swirling and non-swirling impinging turbulent jets

机译:旋流和非旋流冲击湍流射流的传热特性

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The effect of swirl on the impingement surface heat transfer is experimentally investigated in incompressible turbulent (Re = 11,600-35,000) impinging air jets. A swirl nozzle (D = 40mm) is used for seamless transition from a non-swirling (S = 0) jet to a highly swirling (S = 1.05) jet. The effect of swirl number (S), nozzle-to-plate distance (H) and Reynolds number (Re) on the radial uniformity and intensity of convective heat transfer on a heated thin foil is examined over the range H = 1D-6D. The use of low-to-medium swirl numbers (S = 0.27-0.45) at Re = 35,000 is found to improve the magnitude of heat transfer (Nu) in the impingement region compared to non-swirling (S = 0) jets over H ≤ 4D. When S further increases, significant enhancement in Nu occurs only at near-field impingement (H ≤ 2D), regardless of the impingement area (footprint). Larger nozzle-to-plate distance (H ≥ 4D) is found to be detrimental on the convective heat transfer, with a significant reduction of Nu intensity. In relation to spatial uniformity of heat transfer, imparting low values of swirl does not appreciably improve Nu uniformity compared to non-swirling jets over all the impingement distances (H) investigated. In contrast, a marked improvement in Nu uniformity (i.e. flat Nu profiles) on the impingement surface occurs for strongly swirling jets (S = 0.77 and 1.05), but only at H = 4D and 6D. The highest Nu regions are found to correlate well with Nu_(rms). The magnitude of Nu significantly reduces across the imaged radial domain as Re decreases, and the relationship appears to be Nu(r)αRe~(0.47). It appears that a transitional swirl number (dependent on Re) exists which controls the impingement heat transfer characteristics.
机译:在不可压缩的湍流(Re = 11,600-35,000)撞击空气射流中,实验研究了涡旋对撞击表面传热的影响。旋流喷嘴(D = 40mm)用于从无旋流(S = 0)射流无缝过渡到高旋流(S = 1.05)射流。在H = 1D-6D的范围内,研究了旋流数(S),喷嘴到板的距离(H)和雷诺数(Re)对加热的薄箔上径向均匀性和对流传热强度的影响。发现在Re = 35,000时使用中低旋流数(S = 0.27-0.45)与在H上进行非旋流(S = 0)的射流相比,可以改善撞击区域的传热(Nu)幅度。 ≤4D。当S进一步增加时,Nu仅在近场碰撞(H≤2D)时才会显着增强,而不管碰撞区域(足迹)如何。发现较大的喷嘴到平板距离(H≥4D)对对流传热有害,Nu强度显着降低。关于传热的空间均匀性,在所有研究的撞击距离(H)上,与无旋流的射流相比,赋予低涡旋值不会明显改善Nu的均匀度。相反,对于强涡旋射流(S = 0.77和1.05),在撞击表面的Nu均匀性(即平坦的Nu轮廓)有显着改善,但仅在H = 4D和6D时才发生。发现最高的Nu区域与Nu_(rms)良好相关。随着Re的减小,Nu的大小在成像的径向域上显着减小,并且该关系似乎为Nu(r)αRe〜(0.47)。似乎存在一个过渡涡旋数(取决于Re),它控制着冲击传热特性。

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