首页> 外文期刊>Applied thermal engineering: Design, processes, equipment, economics >Effect of offset-jets arrangement on leading edge hot-air heating effectiveness of engine inlet guide strut
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Effect of offset-jets arrangement on leading edge hot-air heating effectiveness of engine inlet guide strut

机译:偏移喷射器布置对发动机入口引导支柱前缘热空气加热效能的影响

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An experimental investigation is conducted to study the effect of offset-jets arrangement on the conjugated heat transfer performance for a specifically wedge-shaped concave surface subjected to external cold flow and internal hot jet impingement. The external flow Reynolds number (Re-c) defined on the base width of wedge-shaped concave surface is fixed as 54,000. The jet Reynolds number (Re-j) is varied in the range of 7900-31,700. Four non-dimensional jet-bole offset distances (L/d) ranging from 0 to 2.5 and four non-dimensional jet-to-leading edge distances (H/d) ranging from 6 to 15 are considered respectively. In order to illustrate the effect of offset-jets arrangement on the flow and heat transfer features inside the wedge-shaped concave cavity, numerical simulations are also performed. The results show that the offset-jets arrangement generally has a significant impact on improving the overall heating effectiveness in the vicinity of concave wall leading edge due to the reduction of normal jet impinging distance and the formation of recirculation flow structure inside the concave cavity. In current study, L/d = 1.5 is confirmed to be a superior offset-jets arrangement for achieving the highest specified area-averaged heating effectiveness. It is also noted that the effect of offset-jets arrangement on the leading edge hot-air heating effectiveness is tightly dependent on the normal jet-to-leading edge distance. Under Hid = 15, the offset-jets distance has a weak effect of on the internal hot-jet impingement heat transfer. In this situation, the offset-jets arrangement has nearly no effect on improving the hot-jet heating effectiveness. (C) 2017 Elsevier Ltd. All rights reserved.
机译:进行实验研究以研究偏移 - 喷射器布置对特异性楔形凹面的共轭传热性能的影响,以进行外部冷流和内部热喷射冲击。在楔形凹面的基础宽度上定义的外部流雷诺数(RE-C)固定为54,000。喷射雷诺数(RE-J)在7900-31,700的范围内变化。分别考虑从0到2.5的0到2.5和四个非尺寸射流到前沿(H / d)的四个非维射流偏移距离(L / D)被考虑为6至15。为了说明偏移 - 喷射装置对楔形凹空腔内的流动和传热特征的影响,还执行数值模拟。结果表明,由于正常喷射撞击距离的降低以及凹腔内的再循环流动结构的形成,偏移喷射器布置通常对提高凹入壁前缘附近的整体加热效能产生显着影响。在目前的研究中,L / D = 1.5被证实是用于实现最高特定区域平均加热效果的优异偏移喷射装置。还应注意,偏移喷射器布置对前缘热空气加热效果的影响紧紧地取决于正常的射流到前沿距离。在HID = 15下,偏移喷射距离对内部热喷射冲击传热具有弱效果。在这种情况下,偏移喷射器布置几乎没有对改善热喷射加热效果的影响。 (c)2017 Elsevier Ltd.保留所有权利。

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