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Conjugate CFD analysis of three trailing-edge cooling configurations.

机译:对三种后缘冷却配置进行CFD分析。

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摘要

Conjugate CFD analyses based on the shear-stress-transport turbulence model were used to study three coolant-passage configurations for the trailing edge: Triple Impingement, Multi-Mesh, and Zig-Zag. All configurations were studied under engine-relevant conditions with a back pressure of 25 bar, external hot-gas temperature of 1,755 K, and coolant temperature at the trailing-edge inlet of 673 K. Parameters investigated include the heat-transfer coefficient on the hot-gas side of the trailing edge (2,000, 4,000, and 6,000 W/m2-K) and the pressure drop across the trailing edge (1 to 5 bar). Results are presented that show the flow induced by each configuration and how that flow affects the surface heat transfer and pressure drop. Also, the performance of the three configurations was compared.;For a given pressure drop, the Triple-Impingement configuration has the second lowest cooling flow rate because of the area constrictions in the flow passage to form the jets for jet impingement. Also, it has the lowest heat transfer rate despite the three jet impingements. The Multi-Mesh has the lowest cooling flow rate but the second highest heat-transfer rate because it has the highest surface area for heat transfer. The Zig-Zag has the highest cooling flow rate because there is little resistance in the flow passage and the highest heat-transfer rate because the cooling flow rate is so high. For a given cooling flow rate, the Multi-Mesh has the highest pressure loss and the highest heat-transfer rate because it has the highest surface area for friction and heat transfer. Zig-Zag has the lowest pressure loss and the second highest heat-transfer rate. Triple Impingement has higher pressure drop than Zig-Zag, but lower heat-transfer rate.;The Multi-Mesh configuration was found to achieve the highest cooling with the lowest cooling flow. For a given mass flow rate, the Multi-Mesh is about 5% better than Zig-Zag and 10% better than Triple Impingement in the amount of heat transferred. For a given pressure drop, the Zig-Zag configuration is the best design because it has the lowest pressure loss and so will yield the highest heat-transfer rate from the highest cooling flow rate unless high cooling flow is undesirable. For a given pressure drop, the Zig-Zag is about 30% better in heat transfer than Triple Impingement and the Multi-Mesh, but uses about 100% more cooling flow rate than does Multi-Mesh and Triple Impingement.
机译:基于剪切应力-传输湍流模型的共轭CFD分析用于研究后缘的三种冷却剂通道配置:三重冲击,多网格和之字形。在与发动机相关的条件下对所有配置进行了研究,背压为25 bar,外部热气温度为1,755 K,后缘入口处的冷却液温度为673K。研究的参数包括热流的传热系数。后缘的气体侧(2,000、4,000和6,000 W / m2-K)和整个后缘的压降(1至5 bar)。给出的结果显示了每种配置引起的流动以及该流动如何影响表面传热和压降。此外,还比较了这三种配置的性能。在给定的压降下,三重配置具有第二低的冷却流速,这是因为在流道中形成用于射流冲击的射流的区域收缩所致。而且,尽管有三个喷射冲击,它的传热率最低。多筛网的冷却流量最低,但传热率第二高,因为它的传热表面积最大。之字形之所以具有最高的冷却流速,是因为在流动通道中阻力很小,而由于冷却流速如此之高,所以传热速率最高。对于给定的冷却流量,多网具有最高的压力损失和最高的传热速率,因为它具有最大的摩擦和传热表面积。之字形的压力损失最低,传热速率第二高。三重撞击比Zig-Zag具有更高的压降,但传热速率更低。;多网状配置可实现最高的冷却效率和最低的冷却流量。对于给定的质量流量,在传热量方面,Multi-Mesh比Zig-Zag好大约5%,比Triple Impingement好10%。对于给定的压降,之字形配置是最佳设计,因为它具有最低的压力损失,因此除非有高的冷却流量,否则会从最高的冷却流量中获得最高的传热率。对于给定的压降,Zig-Zag的传热性能要比三重冲击和多网孔好30%,但比多网眼和三重冲击时多使用约100%的冷却流量。

著录项

  • 作者

    Liu, Jason.;

  • 作者单位

    Purdue University.;

  • 授予单位 Purdue University.;
  • 学科 Engineering Aerospace.;Engineering Mechanical.
  • 学位 M.S.A.A.
  • 年度 2013
  • 页码 73 p.
  • 总页数 73
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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