...
首页> 外文期刊>Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics >Conjugate heat transfer on full-coverage film cooling with array jet impingements with various Biot numbers
【24h】

Conjugate heat transfer on full-coverage film cooling with array jet impingements with various Biot numbers

机译:在全覆盖薄膜冷却中的共轭传热,阵列喷射射流与各种Biot数

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

Total cooling effectiveness was determined on a film cooled surface with staggered array jet impingement cooling at various Biot numbers. Heat transfer experiments were conducted using infra-red thermography for materials of three thermal conductivities: stainless steel (k = 13.4 W/m K), Corian (k = 1 W/m K), and polycarbonate (k = 0.2 W/m K). Conjugated heat transfer was analyzed with the combined effects of conduction through the test plates and convective heat transfer due to the arrayed jet impingement. The inclination angle of the film cooling holes was 35 and that of the jet impingement holes was 90. The film and jet impingement holes on each plate were arranged in staggered patterns, and the film cooling holes and jet impingement holes were also positioned in a staggered pattern. The jet Reynolds number, based on hole diameter, was 3000 and the equivalent blowing ratio was 0.3. The diameter of the film cooling holes and the jet impingement holes was 5 mm. The distance between jet and film hole plates was varied in the range 1 <= H/d <= 5. Total cooling effectiveness was measured with and without jet impingement. When jet impingement was added to the internal cooling, the averaged total cooling effectiveness was enhanced about 8.4%. At low Biot numbers, meaning that cooling performance dominated over the conduction effect, the temperature distribution became more uniform due to higher conductive heat transfer. The total cooling effectiveness was strongly related to the Biot number of the plate, and the correlation between total cooling effectiveness at various Biot numbers was determined to predict the total cooling effectiveness in an actual gas turbine engine. The effect of Hid ratio was limited, to within 2.7%. (C) 2016 Elsevier Inc. All rights reserved.
机译:在薄膜冷却表面上测定总冷却效果,其在各种Biot数处具有交错的阵列喷射冲击冷却。使用红外线热成像进行传热实验,用于三种热导体的材料:不锈钢(k = 13.4W / m k),Corian(k = 1w / m k)和聚碳酸酯(k = 0.2 w / m k )。通过通过测试板的传导和由于阵列喷射撞击引起的对流热传递来分析共轭传热。膜冷却孔的倾斜角度为35,喷射冲击孔的倾斜角度为90.在每个板上的薄膜和喷射冲击孔以交错的图案布置,并且薄膜冷却孔和喷射冲击孔也定位成交错图案。喷射雷诺数基于孔直径为3000,等效的吹出比为0.3。薄膜冷却孔的直径和喷射冲击孔为5mm。射流和薄膜孔板之间的距离在1 <= H / D <= 5的范围内变化。用射流冲击测量总冷却效果。当加热喷射冲击到内部冷却时,平均总冷却效果增强约8.4%。在低生物数据中,这意味着由于导电热传递更高的导电性传热,温度分布变得更加均匀。总冷却效果与板的Biot数密切相关,并确定各种生物数据的总冷却效能之间的相关性以预测实际燃气涡轮发动机中的总冷却效果。 HID比率的影响有限,在2.7%以内。 (c)2016年Elsevier Inc.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号