期刊文献+

超临界压力RP-3起始加热段传热恶化数值研究 被引量:5

Numerical Study on Heat Transfer Deterioration in the Initial Heating Region of RP-3 Under Supercritical Pressure
原文传递
导出
摘要 使用开源流体动力学程序库OpenFOAM对竖直圆管内超临界压力RP-3对流传热进行数值模拟,研究重点为起始加热段的传热恶化现象。本文选择k-ε-v^2-f和k-ωSST两种低Re数湍流模型进行计算并与实验数据进行对比,讨论了两种模型对于高壁面热流条件下传热恶化现象的预测能力.通过对流场及温度场的分析对起始加热段传热恶化现象给出机理解释,最后考察了变物性及浮升力的影响。结果表明:k-ωSST模型无法模拟传热恶化;k-ε-v^2-f模型能够定性描述起始加热段内壁温的迅速升高。由流体密度变化及重力引起的浮升力作用是导致起始加热段传热恶化的重要原因。 The open source CFD toolbox OpenFOAM was used to simulate convective heat transfer of RP-3 flowing in a vertical tube under supercritical pressure. Heat transfer deterioration(HTD)in the initial heating region was studied. Two types of low-Reynolds number turbulence models(k-ε-v^2-f and k-ω SST model) were used in the simulation. Numerical results were compared against the experimental data to examine the accuracy of turbulence models in predicting HTD under large wall heat fluxes. The flow field and temperature field were analyzed to propose a mechanism for explaining HTD. The effects of property variations and buoyancy forces were also investigated.It was concluded that the k-ω SST model was incapable to predict HTD. The k-ε-v^2-f model was able to qualitatively describe the rapid increase of inner wall temperature in the initial heating region. The buoyancy forces caused by density variation and gravity is the main cause of HTD.
作者 浦航 李素芬 东明 尚妍 焦思 PU Hang LI Su-Fen DONG Ming SHANG Yan JIAO Si(Key Laboratory of Ocean Energy Utilization and Energy Conservation of Ministry of Education, Dalian University of Technology, Dalian 116024, China)
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2017年第10期2242-2248,共7页 Journal of Engineering Thermophysics
基金 国家自然科学基金资助项目(No.51576027)
关键词 超临界压力流体 对流换热 数值计算 RP-3 supercritical pressure fluid convective heat transfer numerical computation RP-3
  • 相关文献

参考文献4

二级参考文献27

  • 1ZHONG FengQuan,FAN XueJun,YU Gong,LI JianGuo.Thermal cracking of aviation kerosene for scramjet applications[J].Science China(Technological Sciences),2009,52(9):2644-2652. 被引量:19
  • 2范学军,俞刚.大庆RP-3航空煤油热物性分析[J].推进技术,2006,27(2):187-192. 被引量:112
  • 3孙青梅,米镇涛,张香文.吸热型碳氢燃料RP-3仿JP-7临界性质(t_c、p_c)的测定[J].燃料化学学报,2006,34(4):466-470. 被引量:33
  • 4Brad H,Michael K.Enhancement of heat transfer andelimination of flow oscillations in supercritical fuels[R].Cleveland,OH:34th AIAA/ASME/SAE/ASEE JointPropulsion Conference and Exhibit,1998.
  • 5Brad H,Michael K.Experimental investigation of heattransfer and flow instabilities in supercritical fuels[R].Se-attle,WA:33rd AIAA/ASME/SAE/ASEE Joint Propul-sion Conference and Exhibit,1997.
  • 6Hines W S,Wolf H.Pressure oscillations associated withheat transfer to hydrocarbon fluid at supercritical pres-sures and temperatures[J].American Rocket Society Jour-nal,1962,32(3):361-366.
  • 7Linne D L,Meyer M L,Braun D C.Investigation of insta-bilities and heat transfer phenomena insupercritical fuels athigh heat flux and temperatures[R].Huntsville,AL:36thAIAA/ASME/SAE/ASEE Joint Propulsion Conferenceand Exhibit,2000.
  • 8DENG Hongwu,ZHANG Cunben,XU Guogiang,et al.Density measurements of endothermic hydrocarbon fuel atsub-and supercritical conditions[J].Journal of Chemicaland Engineering Data,2011,56(6):2980-2986.
  • 9ZHANG Cunben,TAO Zhi,XU Guoqiang,et al.Heattransfer invest igation of the sub-and supercritical fuel flowthrough a U-turn tube[R].Antalya,Turkey:Turbine-09,the ICHMT Int.Symposium on Heat Transfer in Gas Tur-bine Systems,2009.
  • 10Jackson J D,Cotton M A,Axcell B P.Studies of mixedconvection in vertical tubes[J].International Journal ofHeat Fluid Flow,1989,10(1):2-15.

共引文献49

同被引文献40

引证文献5

二级引证文献16

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