冲击粗糙壁面复合冷却实验研究
Experimental Investigation on Impingement Heat Transfer from Rib Roughened Surface
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摘要: 对有初始横流的冲击粗糙壁面复合冷却技术进行了实验研究。由以往研究可知,影响换热效果的因素很多,主要可分为流动参数和几何参数。本文主要通过实验以了解各种流动参数、几何参数对换热特性的影响规律,并对其结构设计提出有价值的参考意见。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 heat transfer from rib roughened surface with two-dimensioned arrays of circular jet with initial crossflow has been investigated experimentally.Through the thousands of experimental data,the effect of the several flow parameters ( Re j=7000~15000,G c/Gj =0~0 5) and geometric parameters ( Xn=5~15,Zn=1 5~5,p/e=5~12,e/d =0 5~1 5) on heat transfer characteristics has been studied.It would be useful for the cooling analysis and design of gas turbine hot section.
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Key words:
- impingement cooling /
- heat transfer /
- experiment
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