对不同多行冷却孔配置的薄膜冷却性能分析
Devendra Pratap Singh1, Veasna Mom2, Sathi Rajesh Reddy3
1Department of Mechanical Engineering, Shiv Nadar Institution of Eminence (Deemed to be University), Greater Noida, 201314, India.
的风扇形孔提供了优越的薄膜冷却效率. 然而,在高速和高流量时,流量分离会导致冷却液分布不对称,显著降低冷却性能.
科学领域:
- 航空航天工程 航空航天工程
- 机械工程 机械工程
- 计算流体动力学的流体动力学.
背景情况:
- 薄膜冷却对于高温燃气轮机组件的热保护至关重要.
- 优化冷却孔几何形状对于提高热屏障效率至关重要.
- 了解各种操作条件下的流动动态是提高燃气轮机性能的关键.
研究的目的:
- 在平面板上研究不同孔配置的薄膜冷却性能.
- 分析主流马赫数和吹风比对冷却效率的影响.
- 开发一种方法来计算冷却液在进口处的总压力.
主要方法:
- 使用OpenFOAM计算流体动力学 (CFD) 平台进行数值模拟.
- 研究了五种不同的冷却孔配置,包括圆柱形和风扇形设计.
- 在0.2和0.5的马赫数和0.5,0.5,1.0和1.5.5的吹比率进行模拟.
主要成果:
- 渐变的风扇形孔配置始终表现出最高的冷却效率.
- 在马赫0.5和1.5的吹风比,风扇形孔显示由于流量分离,冷却液分布不对称.
- 这种不对称性导致与相同吹风比的圆柱形孔相比,对分层的风扇形孔的平均薄膜冷却效率减少了60%左右.
结论:
- 风扇形孔提供优越的薄膜冷却,但它们的性能对流量条件敏感.
- 在高马赫数和吹风比率的风扇形通道中的流量分离显著降低了冷却效率.
- 提出的数学方程有助于为薄膜冷却模拟设置准确的入口边界条件.
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