研究了具有尾缘槽缝和多排复杂冷气喷射进口弯掠导叶的气膜冷却特性,所研究的叶片具体有2个冷却腔,尾缘劈缝与副冷却腔相连,表面总共布置有11排冷气喷射孔,给出了多孔气膜冷却叶片几何构造和网格生成的过程.给出了不同湍流度下叶片中部区域叶片型线上的压力系数和速度比分布情况,并讨论了各个位置上的分布特点.探讨了在内表面换热和外表面气膜覆盖条件下,压力面和吸力面上展向的平均实际气膜冷却效率沿流向的分布特点,并且对各自冷却特点进行了分析.
参考文献
[1] | Mehendale A B;Ekkad S V et al.Main Stream Turbulence Effect on Film Cooling Effectives of a Gas Turbine Blade with Air and CO2 Film Injection[J].International Journal of Heat and Mass Transfer,1994,37:2707-2714. |
[2] | Jiang H W;Han J C et al.Effect of Film Hole Row Location on Film Effectives on a Gas Turbine Blade[J].ASME Journal of Heat Transfer,1996,118:327-333. |
[3] | Ou S;Han J C et al.Unsteady Wake on a Linear Turbine Blade Cascade with Air and CO2 Film Injection:Part 1-Effect on Heat Transfer Coefficients[J].ASME Journal of Turbine Machinery,1994,116:721-729. |
[4] | Mehendale A B;Han J C et al.Unsteady Wake on a Linear Turbine Blade Cascade with Air and CO2 Film Injection:Part 1-Effect on Film Effectives and Heat Transfer Distributions[J].ASME Journal of Turbine Machinery,1994,116:730 737. |
[5] | C W Haldeman;R M Mathison.Aerodynamic and Heat Flux Measurements in a Single Stage Fully Cooled Turbine:Part Ⅰ-Experimental Approach[A].,2006 |
[6] | C W Haldeman;R M Mathison.Aerodynamic and Heat Flux Measurements in a Single Stage Fully Cooled Turbine:Part Ⅱ-Experimental Results[A].,2006 |
[7] | Shantanu Mhetras;Je-Chin Han.Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a GasTurbine Blade[A].,2007 |
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