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角度和孔间距对双向扩张型孔流量系数影响的实验
引用本文:李广超,朱惠人,樊慧明.角度和孔间距对双向扩张型孔流量系数影响的实验[J].航空动力学报,2009,24(3):499-506.
作者姓名:李广超  朱惠人  樊慧明
作者单位:西北工业大学动力与能源学院,西安,710072
摘    要:为了研究非常规扩张孔的流动特性,测量了一排7个双向扩张孔的平均流量系数.气膜孔的前倾角为20°,45°和90°,径向角为0°,30°和65°,孔间距与孔径比为2,3和4.动量比变化范围为1到8.结果表明,径向角为0°的流量系数随前倾角的增加显著增加.前倾角为20°的流量系数随径向角的增加略有减小.前倾角为90°的流量系数随孔间距的增加而增加.

关 键 词:涡轮叶片  气膜冷却  流量系数  实验
收稿时间:2/29/2008 4:09:15 PM
修稿时间:7/14/2008 2:26:34 PM

Influence of angles and hole pitches on discharge coefficients of expanded holes at inlet and outlet
LI Guang-chao,ZHU Hui-ren and FAN Hui-ming.Influence of angles and hole pitches on discharge coefficients of expanded holes at inlet and outlet[J].Journal of Aerospace Power,2009,24(3):499-506.
Authors:LI Guang-chao  ZHU Hui-ren and FAN Hui-ming
Institution:School of Engine and Power;Northwestern Polytechnical University;Xi'an 710072;China
Abstract:This paper presented discharge coefficients of the expanded holes at inlet and outlet with plane angles of 20°,45°,90°,radial angles of 0°,30°,65° and the ratios of pitch to diameter of 2,3,4.The momentum flux ratios varied in the range from 1 to 8.The results show that discharge coefficients of radial angle =0° increase significantly when the plane angles increase from 20° to 90°.The effect of plane angle becomes weak with the increasing radial angles.Radial angles have weak influence on the discharge coefficients of plane angle=20° and discharges coefficients of plane angle=45°and plane angle=90° decreases when the radial angles increase from 0° to 65°.Discharge coefficients of plane angle=90°increase when the ratios of hole pitch to the diameter increase from 2 to 4.
Keywords:turbine  film cooling  discharge coefficient  experiment  
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