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首页> 外文期刊>Defence science journal >Comparative Performance of New Surface Roughness Element and Pin fin in Converging Channel for Gas Turbine Application
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Comparative Performance of New Surface Roughness Element and Pin fin in Converging Channel for Gas Turbine Application

机译:新型表面粗糙度元件和销料在燃气轮机应用中换气通道的比较性能

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Thermal performance of a novel surface roughness element, named as Double 45 Dimple (D45D), is compared with pin-fin element in a converging channel with rectangular cross section and presented. The Surface Roughness Element (SRE) is derived by combining protrusion & dimple in a particular fashion such that area available for transfer of heat increases. The objective of this study is to demonstrate the applicability of D45D element channel for trailing edge channel of a typical nozzle guide vane where typically pin-fin element is used. New cooling configuration of Nozzle Guide Vane (NGV) with D45D element is also proposed. All thermal and flow related results are derived using validated CFD approach with EARSM turbulence model for a typical value of Reynolds number. From this investigation, it is found that D45D element provides remarkable improvement in the averaged as well as heat transfer in local region for the corresponding surface which makes it a candidate for trailing edge channel cooling application.
机译:将命名为双45瓣(D45D)的新型表面粗糙度元件的热性能与具有矩形横截面的会聚通道中的销翅片元件进行比较。表面粗糙度元件(SRE)通过以特定方式组合突起和凹斑而导出,使得可用于传递热量的区域增加。本研究的目的是展示D45D元件通道用于典型喷嘴导向叶片的后缘通道的适用性,其中通常使用销鳍元件。还提出了具有D45D元件的喷嘴导向叶片(NGV)的新冷却结构。所有热和流量相关结果都是使用验证的CFD方法来源的,具有耳朵湍流模型,用于雷诺数的典型值。从该研究开始,发现D45D元件在局部区域的平均值中提供了显着的改进,用于相应的表面,这使其成为用于后缘通道冷却应用的候选者。

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