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首页> 外文期刊>International Journal of Thermal Sciences >Convective heat transfer by a row of tab-excited impinging jets on a wedge-shaped concave surface
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Convective heat transfer by a row of tab-excited impinging jets on a wedge-shaped concave surface

机译:在楔形凹面上通过一排片状激发射流进行对流传热

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A Computational study was conducted to investigate the convective heat transfer characteristics by a row of tab-excited air jets impingement on a wedge-shaped concave surface having larger curvature than semi-circular concave surface. The geometric effects, including the tab number and tab penetration ratio, as well as the offset-jets arrangement, on the impinging jet flow and heat transfer behaviors are analyzed under several non-dimensional jet-to-leading edge distances (6, 9, 12) and the jet Reynolds numbers ranging from 6900 to 26,100. The results show that both the jet offset-arrangement and tab-excitation are proved to be capable of improving the convective heat transfer in the vicinity of jet impingement region. Either for the conventional round jet or tab-excited jet, it appears that an optimum non-dimensional jet-offset distance is about 1.5. The heat transfer enhancement is improved as the increase of tab number (ranging from 4 to 8), as well as tab penetration ratio (ranging from 0.13 to 0.25). The influence intensity of non-dimensional jet-offset distance on the convective heat transfer inside a concave cavity is more significant for the tab-excited jet impingement than that for the conventional round jet impingement. In general, the effects of jet offset-arrangement and tab-excitation on the jet impingement heat transfer enhancement behave more significant under larger jet Reynolds number as well as smaller impingement distance. (C) 2015 Elsevier Masson SAS. All rights reserved.
机译:通过计算研究来研究对流传热特性,该行为是通过将一排片状激发空气射流撞击到曲率比半圆形凹面大的楔形凹面上来进行的。在几个无量纲的射流到前沿距离的情况下(6、9、9),分析了包括突片数量和突片穿透率以及偏置射流布置对撞击射流和传热行为的几何影响。 12),喷气式雷诺数从6900到26,100。结果表明,射流偏移布置和翼片激励都被证明能够改善射流撞击区域附近的对流传热。对于常规的圆形射流或翼片激发射流,似乎最佳的无量纲射流偏移距离约为1.5。随着接片数量的增加(从4到8)以及接片穿透率(从0.13到0.25),传热增强得到改善。与常规的圆形射流冲击相比,对于片式激发射流冲击,无量纲射流偏移距离对凹腔内部对流传热的影响强度更为显着。通常,在较大的射流雷诺数和较小的射流距离下,射流偏移布置和翼片激励对射流冲击传热增强的影响更为显着。 (C)2015 Elsevier Masson SAS。版权所有。

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