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本文对开槽前扩孔及在此基础上加30°、45°和60°不同角度复合角的气膜冷却结构进行了数值模拟,计算了指定冷却壁面的温度场分布以及冷却效率.结果表明:引入复合角后,能够改善冷却气膜在壁面的横向分布,复合角越大,气膜分布越均匀.在高吹风比下,复合角结构能够产生较大的气膜覆盖范围和较好的冷却效果.

Numerical simulation technique is used to investigate the effects of a compound angle (30°,45°or 60°)on the film cooling performance based on a trench-shaped hole geometry.From the film cooling efficiency and velocity distribution,the results indicate that the compound angle can improve the lateral coverage of cooling film over a hot surface.Moreover,with the increase of the compound angle,the cooling film shows considerable uniform cover and better cooling performance,especially at a high blowing ratio.

参考文献

[1] S K Waye;D G Bogard .High Resolution Film Cooling Effectiveness Measurements of Axial Holes Embedded in a Transverse Trench with Various Trench Configurations[ASME Paper GT-2006-90226][R].,2006.
[2] Y P Lu;A Dhungel;S V Ekkad et al.Effect of Trench Width and Depth on Film Cooling from Cylindrical Holes Embedded in Trenches[ASME Paper GT2007-27388][R].,2007.
[3] D. L. Schmidt;B. Sen;D. G. Bogard .Film cooling with compound angle holes: adiabatic effectiveness[J].Journal of turbomachinery,1996(4):807-813.
[4] A K Sinha;D G Bogard;M E Crawford .Film-Cooling Effectiveness Downstream of a Single Row of Holes with Variable Density Ratio[J].ASME Journal of Turbomachin-ery,1991,113:42-449.
[5] D R Pedersen;E R Eckert;R J Goldstein .Film Cooing with Large Density Differences Between the Main-stream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy[J].ASME Journal of Heat Transfer,1977,99:620-627.
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