期刊文献+

变物性与热辐射对发汗冷却过程的影响规律研究 被引量:4

Influence of Variable Thermophysical Properties and Thermal Radiation on Convection Heat Transfer in Transpiration Cooling
下载PDF
导出
摘要 采用两层k-ε湍流模型对高温条件下有发汗冷却时的矩形槽道内湍流流动和换热进行了数值模拟。计算结果表明:随着冷却气体流量的增加,在发汗冷却壁面附近主流气体的温度梯度大大减小,壁面温度、局部对流换热系数都迅速下降;变物性条件下同时考虑热辐射时数值计算得到的平均St相对值(St/St0)随修正注入率F/St0的变化比已知的常物性条件下的值小;随着高温气体温度的上升,变物性和热辐射对与高温流体接触的表面温度有较大影响,热辐射对壁面温度的影响比变物性更大,而对流换热系数所受的影响不大;当主流为高温气体(如:2500K)、而壁面温度较低时(如:800K)热辐射的影响不大,发汗冷却效果仍然很明显。 The two-layer k-ε model was used to calculate the turbulent flow and heat transfer characteristics in a rectangular channel with transpiration cooling.The calculated results showed that increasing cooling flow rate greatly reduced the wall temperature,the local convection heat transfer coefficient and the temperature gradient in the main flow near the transpiration cooling wall.The changes of the ratio of St/St_0 for various values of the modified blowing ratio F/St_0 for variable thermophysical properties with consideration of thermal radiation were less than the changes for constant properties.Increases of the main flow temperature increased the effect of the variable properties and thermal radiation.The influence of thermal radiation on the wall temperature was stronger than the influence of variable thermophysical properties.The influence of the variable properties and thermal radiation on the convection heat transfer coefficient was small.When the main flow temperature was high (e.g.2500 K) and the wall temperature was low (e.g.800 K),the effect of the thermal radiation was not strong and the transpiration cooling effect was still obvious.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2004年第2期184-190,共7页 Journal of Aerospace Power
基金 国家杰出青年科学研究基金(50025617)
关键词 变物性 热辐射 发汗冷却 影响规律 数值模拟 比冲 aerospace propulsion system transpiration cooling numerical simulation turbulence variable thermophysical properties thermal radiation
  • 相关文献

参考文献16

  • 1Yanovski L S. Physical Basis of Transpiration Cooling for Engines of Flying Apparatus[M]. Moscow.. MAI Press, 1996.
  • 2Chen F, Bowman W J. Effect of Transpiration Cooling on Nozzle Heat Transfer [J]. J- Spacecraft, Engineering Notes,1995,33(3) :453-455.
  • 3Reddy N M. Transpiration Cooling Analysis at Hypersonic Mach Numbers by Using Navier-Stokes Equations[A]. 6th AIAA/ASME Joint Thermophysics and Heat Transfer Conference[C]. 1994: 20- 23.
  • 4Landis J A,Bowman W J. Numerical Study of a Transpiration Cooled Rocket Nozzle[A]. 32nd AIAA/ASME/SAE/ASEEJoint Propulsion Conference[C]. 1996:11 - 15.
  • 5Yan W M,Tzeng P Y. Transport Phenomena of Developing Laminar Mixed Convection in Inclined Rectangular Ducts With Wall Transpiration [J]. Transactions of the ASME,2001,123:121 - 127.
  • 6Bellettre J,Bataille F,Lallemand A. A New Approach for the Study of Turbulent Boundary Layers with Blowing[J]. International Journal of Heat and Mass Transfer, 1999, 42:2905-2920.
  • 7Launder B E,Spalding D B. The Numerical Computation of Turbulent Flows [J]. Comp. Math. in Appl. Mech. and Eng. ,1974,3:269.
  • 8Kays W M, Crawford M E. Convective Heat and Mass Transfer[M]. (2d ed. )New York:McGraw- Hill, 1980.
  • 9刘国球.液体火箭发动机原理[M].北京:宇航出版社,1993..
  • 10姜培学,任泽霈,张左匆,陈旭扬.液体火箭发动机推力室发汗冷却传热过程的数值模拟 (Ⅰ)数理模型[J].推进技术,1999,20(3):1-4. 被引量:13

二级参考文献13

  • 1刘伟强,中国工程热物理学会第七届全国学术会议论文集,1998年,377页
  • 2Jiang Peixue,J Therm Sci,1996年,15卷,1期,43页
  • 3刘国球,液体火箭发动机原理,1993年
  • 4张远君,流体力学大全,1991年
  • 5Yanovski L S. Physical Basis of Transpiration Cooling for Engines of Flying Apparatus [M]. Moscow: MAI Press,1996.
  • 6Launder B E, Spalding D B. The numerical computation of turbulent flows [J]. Comp Math in Appl Mech & Eng,1974, 3: 269-273.
  • 7Rodi W. Experience with two-layer models combining the model with a one-equation model near the wall [A].AIAA-91-0216, 29th Aerospaces Sciences Meeting [C],January 7-10, Nevada, USA, 1991.
  • 8Durbin P A, Medic G, Seo J M, et al. Rough wall modification of two-layer k-ε [J]. J Fluids Engineering,2001, 123: 16-21.
  • 9Lam C K G, Bremhorst K. A modified form of the model for predicting wall turbulence [J]. ASME J Fluids Eng, 1981,103:456 - 461.
  • 10Petukhov B S, Genin L G, Kovalev S A. Heat Transfer in Nuclear Power Equipment [M], Moscow: Energoatomizdat Press, 1986.

共引文献56

同被引文献50

引证文献4

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