期刊文献+

气膜冷却平板通道的数值模拟 被引量:3

Numerical Simulation of a Gas Film-cooled Flat Plate Channel
在线阅读 下载PDF
导出
摘要 对无肋和带45°肋气膜冷却平板通道的三维对流换热与导热耦合传热问题进行了数值模拟。网格划分采用非结构化网格,湍流模型为SSTk-ω模型,近壁处采用壁面函数法,采用SIMPLEC算法求解速度和压力的耦合。计算获得了无肋和带45°肋气膜冷却平板的流场分布和平板内外表面的平均温度和平均换热系数。计算结果表明,带45°肋的气膜冷却平板表面平均温度较无肋气膜冷却平板表面平均温度低,而近气膜孔区域冷、热表面平均换热系数较无肋时高,而且肋的存在对增大冷空气出流比有利。 A numerical simulation was performed of the coupled heat transfer problem involving the three-dimensional convection heat exchange and heat conduction in a gas film-cooled flat plat channel without ribs and with 45o ribs. A non-structured network was adopted for network division. The turbulent flow model is of a SST k-ω one. A wall function method has been adopted for the near-wall location. The coupling of speed and pressure was solved by using a SIMPLEC algorithm. Through calculations obtained were for the gas film-cooled flat plate without ribs and with 45° ribs a flow field distribution and the average temperature and average heat exchange factor at the flat plate inner and outer surface. The calculation results indicate that the channel flow-field structure of the gas film-cooled flat plate with 45° ribs is relatively complicated. The surface average temperature of the flat plate is lower than that of the gas film-cooled flat plate without ribs. However, the cold and hot surface average heat exchange factor near the gas-film pore zone is higher than in the case when no ribs are provided. Furthermore, the presence of ribs is favorable for enhancing cold-air outward flow ratio.
出处 《热能动力工程》 EI CAS CSCD 北大核心 2005年第4期411-413,共3页 Journal of Engineering for Thermal Energy and Power
关键词 气膜冷却 温度 换热系数 数值模拟 出流比 rib, gas film cooling, temperature, heat exchange factor, numerical simulation, outward flow ratio
  • 相关文献

参考文献4

  • 1STEPHENS M A,SHIH T I P,CIVINSKAS K C.Computation of flow and heat transfer in a rectangular channel with ribs[A].33rd Aerospace Sciences Meetings and Exhibit[C].Reno:AIAA,1995.AIAA-95-0180.
  • 2JANG YONG JUN,CHEN HAMN CHING,HAN JE CHIN.Flow and heat transfer in a rotating square channel with 45 deg angled ribs by reynolds stress turbulence model[J].Journal of Turbomachinery of ASME,2001,123(1):124-132.
  • 3CHANTELOUP D,BOLCS A.Flow characteristics in two-leg internal coolant passage of gas turbine airfoils with film-cooling hole ejection[J].Journal of Turbomachinery of ASME,2002,124(7):499-507.
  • 4HAN J C,ZHANG Y M,LEE C P.Augmented heat transfer in square channels withparallel,crossed, and V-shaped angled ribs[J].ASME J Heat Transfer,1991,113:590-596

同被引文献28

  • 1李永康,张靖周,姚玉.利用三角形突片改善气膜冷却效率的数值研究[J].航空动力学报,2006,21(1):83-87. 被引量:21
  • 2李少华,宋东辉,刘建红,王虎,郭婷婷.不同孔型平板气膜冷却的数值模拟[J].中国电机工程学报,2006,26(17):112-116. 被引量:30
  • 3唐婵,常海萍,毛军逵.离散孔纵向波纹隔热屏气膜冷却特性研究[J].工程热物理学报,2007,28(3):487-489. 被引量:12
  • 4Gritsch M, Schulz A, Wittig S. Adiabatic wall effectiveness measurements of film cooling holes with expanded exits [J]. ASME Journal of Turbomachinery, 1998, 120(3).. 549-556.
  • 5韩介勤,等著,程代京,谢永慧译.燃气轮机传热和冷却技术[M].西安:西安交通大学出版社,2005.
  • 6Nasir H, Ekkad S V, Acharya S. Effect of compound angle injection on flat surface film cooling with large stream- wise injection angle[J]. Experimental Thermal and Fluid Science, 2001, 25(1): 23-29.
  • 7Koc I, Parmaksizoglu C, Cakan M. Numerical investigation of film cooling effectiveness on the curved surface[J]. Energy Conversion and Management, 2006, 47(9) : 1231 -1246.
  • 8Wang T, Chintalapati S, Bunker R S, et al. Jet mixing in a slot[J]. Experimental Thermal and Fluid Science, 2000, 22(1): 1-17.
  • 9Bunker R S. Film cooling effectiveness due to discrete holes within a transverse trench [R]. ASME Paper GT2002-30178,2002,
  • 10Lu Y, Nasir H, Ekkad S V. Film cooling from a row of holes embedded in transverse slots [R]. ASME Paper GT2005-68598,2005.

引证文献3

二级引证文献24

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