节点文献
间隙尺寸对涡轮叶栅气动性能影响的实验研究
Experimental Study of the Effect of Blade Tip Clearance on Turbine Performance
【摘要】 测量了较大间隙 (τ =0 .0 36 )下常规直叶栅中分面和上下游及栅内的气动参数 ,并与黄洪雁博士测量的较小间隙 (τ=0 .0 2 3)下相同叶栅的试验数据进行了详细比较 ,讨论了间隙尺寸变化对间隙流动和整体叶栅气动特性的影响
【Abstract】 The airflow parameter in the conventional straight cascade with bigger blade tip clearance(τ=0.036) was measured in detail.The experiment result was compared with that measured by PhD Huang for smaller blade tip clearance(τ=0.023).The effects of tip clearance in clearance flow and blade cascade performance were discussed.
- 【文献出处】 节能技术 ,Energy Conservation Technology , 编辑部邮箱 ,2004年04期
- 【分类号】TK474.71
- 【被引频次】8
- 【下载频次】148