冲击粗糙肋壁面流动特性实验研究
Impingement Fluid Characteristics from Rib Roughened Surface within Arrays of Circular Jet
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摘要: 对有初始横流的冲击粗糙肋壁面的流场进行了流动特性实验研究,通过对大量实验数据的整理、分析以了解多种流动和几何参数对其流动特性的影响规律,为优化设计涡轮叶片内部冷却结构提供相应依据Abstract: Impingement heat transfer is one of the useful cooling methods for high temperature gas turbine blades and/or guide vanes in aeroengines.After the cooling jet impinges on the leading edge of the turbine blade and/or guide vane,it flows downstream and turns to be the initial crossflow for the aft row of impinging jet.The process of impingement heat transfer is quite complicated, especially when the target surface is rib roughened. In this paper,impingement fluid characteristics from rib roughened surface with two dimensional arrays of circular jet with initial crossflow have been investigated experimentally.Through thousands of experimental data,the effect of several flow parameters ( Re j=7000~15000,G c/G j =0~0.5) and geometric parameters ( Xn=5~15,Zn=1 5~5,p/e=5~12,e/d =0 5~1 5) on fluid characteristics has been studied.It would be useful for the design in gas turbine hot section.
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Key words:
- blades /
- flow fields /
- fluid characteristics /
- cooling
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