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Analysis of cooling effectiveness for heat flux based on reference enthalpy

Analysis of cooling effectiveness for heat flux based on reference enthalpy
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摘要 In order to quickly and accurately compute the wall temperature distribution along the combustor axial line, a method to compute the temperature field of combustion chamber with active regeneratively cooling was presented. On the condition of nonstationary wall temperature, the one-dimensional cooling model based on reference enthalpy was established, and the distribution of the wall heat flux and the wall temperature along the combustor axial line were obtained at different mach numbers by using the heat transfer empirical equation. For the existing two types of cooling system structure, the cooling effectiveness of which was investigated through the presented method. And the satisfactory results obtained show the validity of the method. In order to quickly and accurately compute the wall temperature distribution along the combustor axial line, a method to compute the temperature field of combustion chamber with active regeneratively cooling was presented. On the condition of nonstationary wall temperature, the one-dimensional cooling model based on reference enthalpy was established, and the distribution of the wall heat flux and the wall temperature along the combustor axial line were obtained at different mach numbers by using the heat transfer empirical equation. For the existing two types of cooling system structure, the cooling effectiveness of which was investigated through the presented method. And the satisfactory results obtained show the validity of the method.
出处 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2008年第2期215-219,共5页 哈尔滨工业大学学报(英文版)
关键词 自动模拟理论 基准热函 热通量 管理学 reference enthalpy effectiveness heat flux
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参考文献8

  • 1Curran E T.Scramjet engines: the first forty years[].Journal of Propulsion Technology.2001
  • 2Takeshi Kanda,Tetsuo Hiraiwa,Tohru Mitani.Mach 6 testing of a scramjet engine model[].Journal of Propulsion Technology.1997
  • 3Daniau E,Bouchez M.Fuel reforming for scramjet thermal management and combustion optimization[].AIAA/CIRA th International Space Planes and Hypersonic Systems and Technologies.2005
  • 4Takeshi Kanda,Yoshio Wakamatsu.Parametric study of airframe-integrated scramjet cooling requirement[].Journal of Propulsion Technology.1991
  • 5Bertin J J.Hypersonic Aerothermodynamics[]..1994
  • 6Jr Anderson J D.Hypersonic and High Temperature Gas Dynamics[]..1989
  • 7Dirrance W H.Viscous Hypersonic Flow[]..1962
  • 8Takeshi Kanda,Goro Masuya,Yoshio Wakamatsu.Propel- lant feed system of a regeneratively cooled scramjet[].Jour- nal of Propulsion and Power.1991

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