期刊文献+

具有复合角的多斜孔板流量系数研究 被引量:3

Research on the Discharge Coefficient of the Inclined Multi-Hole Plates with Compound Angle
下载PDF
导出
摘要 试验研究了多种结构多斜孔板的流量系数,分析了孔倾角、孔偏角、板厚等几何结构参数,和孔内流动雷诺数、主次流温比、主流马赫数等气动参数对具有复合角的多斜孔板流量系数的影响。研究结果表明:①孔内流动雷诺数小于4 000时,流量系数与雷诺数呈线性关系,大于5 000时流量系数变化不大;②孔偏角小于40°时,流量系数随孔偏角的增大而减小,大于40°时对流量系数的影响不大;③流量系数随板厚及主次流温比的增大而减小,孔内换热量对多斜孔板流量系数的影响较大;④流量系数随主流马赫数的增大而增大。本研究结果对航空发动机燃烧室空气流量分配及冷却设计具有一定的参考价值。 Measurements of discharge coefficients for different configurations of the inclined multi-hole plates with compound angle are presented. The factors affecting the discharge coefficient are discussed such as inclination angle, orientation angle, plate thickness, the Reynolds number, temperature ratio between the main flow and the secondary flow and Mach numbers of the main flow. Results show that linear relationship can be observed when Reynolds number is below 4 000, but more than 5 000 it doesn' t affect discharge co- efficient much; when orientation angle is below 40° the increased orientation angle results in decreased discharge coefficients; the discharge coefficient decreases as the plate thickness and the temperature ratio increases; and the increased Mach number leads to higher discharge coefficient. This study is referential to flow distribution and cooling design of aero-engine combustor.
出处 《燃气涡轮试验与研究》 2011年第4期28-31,共4页 Gas Turbine Experiment and Research
关键词 复合角 多斜孔板 流量系数 几何结构参数 气动参数 compound angle inclined multi-hole plates discharge coefficient configuration parameters aerodynamic parameters
  • 相关文献

参考文献5

  • 1Burd S W, Simon T W. Measurements of Discharge Coeffi- cients in Film Cooling[J]. ASME Journal of Turbomachin- ery, 1999,121:243--248.
  • 2Hay N, Henshall S E, Manning A. Discharge Coefficients of Holes Angled to Flow Direction[J]. ASME Journal of Turbomachinery, 1994,116 : 92--96.
  • 3方韧,林宇震,李彬,刘高恩.燃烧室多斜孔壁流量系数研究[J].航空动力学报,1998,13(1):61-64. 被引量:16
  • 4Gritsch M, Schulz A, Wittig S. Effect of Crossflows on the Discharge Coefficient of File Cooling Holes with Varying Angles of Inclination and Orientatino[R]. ASME 2001-GT-0134,2001.
  • 5张树林,王洪斌.多斜孔板气膜冷却性能试验研究[J].航空发动机,2005,31(3):23-26. 被引量:1

二级参考文献5

  • 1高峰,硕士学位论文,1995年
  • 2Goidstein R J, et al. Film Cooling of a Row of Discrete Holes with Compound Angle. AMSE2001 April, vol. 123~225.
  • 3Sasaki M, et al. Film Cooling Effectiveness for Injection From Multirow Holes. ASME. 2001 April ,vol.123.
  • 4Gritsch M, et al. A Method for Correlating the Discharge Coefficient of Film- Cooling Holes with Crossflows at Hole Entry and Exit. International sysposium on air breathing engines:13th - 1997.9.7 - 121. - 771 - 777. ISABE 97 -7110.
  • 5Roubury D A, et al. A Method for Correlecting the Inflounce of Extrenal Crossflow on the Dischange Coefficient of Film Cooling Holes, AMSE2001 April,vol. 123 ~ 259.

共引文献15

同被引文献21

引证文献3

二级引证文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部