期刊文献+

克努森数对气膜冷却流动换热相似特性的影响 被引量:1

Effect of Knudsen number on similar characteristics of film cooling flow and heat transfer
原文传递
导出
摘要 数值模拟研究克努森数Kn对不同尺度气膜冷却流动换热相似特性的影响,选取孔径为0.3,3,10mm平板单排圆柱形气膜孔模型,计算得到模型在Kn不同与相同条件下冷却效率和孔流量系数.结果表明:Kn相同时,小孔与大孔模型流动换热特性相似,冷却效率及流量系数均吻合很好;Kn不同时,两模型流动换热特性存在一定差异,冷却效率及流量系数吻合较差.因此为在气膜冷却相似放大研究中得到准确的相似结果,需要保证小孔及大孔模型的Kn相同. The effect of Knudsen number Kn on the similar characteristics between different scale film cooling flow and heat transfer was numerically studied. Single-row plate cylindrical hole film cooling models with aperture of 0.3, 3, 10 mm were seleeted. Cooling effectiveness and discharge coefficient of models under condition of different Kn and the same Kn were calculated. Results show that small and large hole models have similar flow and heat transfer characteristics under the same value of Kn, resulting in little differences between cooling effectiveness and discharge coefficient. When Kn varies, the flow and heat transfer characteristics of these two models are different, bringing about different cooling effectiveness and discharge coefficients. Therefore it is necessary to make sure that small and large hole models should have the same Kn in similar amplification experiment of film cooling.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2015年第5期1106-1112,共7页 Journal of Aerospace Power
基金 航空科学基金(2014ZB53023) 国家自然科学基金(51306152) 霍英东教育基金(141053) 中央高校基本科研业务费专项资金(3102014JCQ01049)
关键词 气膜冷却 流动换热相似特性 克努森数 冷却效率 流量系数 film cooling similar characterisitics of flow and heat transfer Knudsen number cooling effectiveness~ discharge coefficient
  • 相关文献

参考文献17

  • 1韩介勤,桑地普·杜达,斯瑞纳斯·艾卡德.燃气轮机传热和冷却技术[M].程代京,谢永慧,译.西安:西安交通大学出版社,2005.
  • 2Leylek J H, Mcgovern K T, Brittingham R A. A detailed a nalysis of film cooling physics.. Part ]][ compound-angle in- jection with cylindrical holes[J]. Journal of Turbomachin- ery,2000,122(1) :113-121.
  • 3Li S J, Yang S F, Han J C. Effect of coolant density on leading edge showerhead film cooling using PSP measure- ment teehnique[R]. ASME Paper GT2013-94198,2013.
  • 4Dong H R,Youn S L,Young B K,et al. Film cooling and thermal field measurements for staggered rows of rectan- gular-shaped film cooling holes[R]. ASME Paper GT2003 38608,2003.
  • 5刘存良,朱惠人,白江涛,许都纯.基于瞬态液晶全表面测量技术的圆柱形孔气膜冷却特性研究[J].航空动力学报,2009,24(9):1959-1965. 被引量:9
  • 6邓宏武,肖俊,李国庆,薛航.吹风比对旋转涡轮叶片气膜冷却的影响[J].航空动力学报,2011,26(7):1452-1457. 被引量:8
  • 7Papautsky I, Ameel T, Frazier A B. A review of laminar single-phase flow in microchannels[R]. New York: ASME International Mechanical Engineering Congress and Expo sition, 2001.
  • 8Kandlikar S G,Colin S, et al. Heat transfer in microchan- nels:2012 status and research needs[J]. Journal of Heat Transfer,2013,135(9) :091001.1-091001.18.
  • 9陶然,权晓波,徐建中.微尺度流动研究中的几个问题[J].工程热物理学报,2001,22(5):575-577. 被引量:66
  • 10Eringen A C. Simple microfluids[J]. International Journal of Engineering Science, 1964,2(2) : 205-217.

二级参考文献48

共引文献155

引证文献1

二级引证文献1

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