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叶片前缘旋流和常规冲击对比数值研究
引用本文:刘高文,薛彪,彭力,夏全忠.叶片前缘旋流和常规冲击对比数值研究[J].推进技术,2011,32(4):576-580,585.
作者姓名:刘高文  薛彪  彭力  夏全忠
作者单位:西北工业大学动力与能源学院,陕西西安,710072
摘    要:为了寻求更好的叶片前缘内冷结构,对旋流冲击和常规冲击的流动和传热特性进行了数值模拟,对比研究了二者的涡流结构、传热强度、流动阻力、综合传热性能和热均匀性,研究了通道Re数和冲击间距对这些参数的影响。结果表明旋流冲击形成的旋涡有利于传热的增强和热均匀性的提高。在所研究的Re数(2×104~7.78×104)和冲击间距(3.3~5倍直径)范围内,旋流冲击与常规冲击相比平均传热增强18%~34%,增幅随Re数和冲击间距的增大而增大;流阻增大10%~26%,增幅随Re数和冲击间距的增大而减小;综合传热性能增强20%左右;热均匀性提高60%左右。

关 键 词:冲击冷却  旋流冲击冷却+  传热系数  流动阻力  热均匀性+
收稿时间:7/8/2010 12:00:00 AM
修稿时间:2010/11/10 0:00:00

Numerical investigation on difference between blade leading edgevortex and normal impingement cooling
LIU Gao-wen,XUE Biao,PENG Li and XIA Quan-zhong.Numerical investigation on difference between blade leading edgevortex and normal impingement cooling[J].Journal of Propulsion Technology,2011,32(4):576-580,585.
Authors:LIU Gao-wen  XUE Biao  PENG Li and XIA Quan-zhong
Institution:(School of Power and Energy,Northwestern Polytechnical Univ.,Xian 710072,China)
Abstract:Numerical simulations for the flow and heat transfer of vortex and normal impingement cooling on the internal channel of blade leading edge were carried out to find better cooling configuration.Comparisons were made between these two cooling forms in such aspects as vortex structure,heat transfer enhancement,pressure loss,thermal performance and thermal uniformity.The influences of Reynolds numbers and spaces between impingement holes on these parameters were studied.Results show that the heat transfer rate...
Keywords:Impingement cooling  Vortex impingement cooling  Heat transfer rate  Pressure loss  Thermal uniformity  
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