Simulation research for radiation heat transfer of engine group by model nozzles

被引:0
|
作者
Cheng, H.-E. [1 ]
Niu, L. [1 ]
机构
[1] Sch. of Power and Energy Engineering, Shanghai Jiaotong Univ., Shanghai 200030, China
来源
关键词
Computer simulation - Heat flux - Heat transfer - Nozzles;
D O I
暂无
中图分类号
学科分类号
摘要
According to the theory of heat radiation, the essential characteristic of outward radiation heat transfer of engine group was researched, and the necessary conditions for simulation research of this heat transfer phenomenon using nozzles, subscale component of electrically heated nozzles were given out to be simialr geometrically, and equal for heat flux q and emissivity Ε on wall surface for the two. Feasibility analysis provides scientific basis for ground simulation test. Its conclusion can be used for guiding the test.
引用
收藏
页码:126 / 128
相关论文
共 50 条
  • [1] Ground simulation test on radiation heat transfer of orbit maneuvering engine group
    Cheng, H.E.
    Niu, L.
    Xu, J.X.
    Pu, B.R.
    Han, H.Y.
    Zhang, Z.G.
    Tuijin Jishu/Journal of Propulsion Technology, 2001, 22 (03): : 207 - 210
  • [2] A numerical simulation on the infrared radiation of hot exhausting nozzles with a coupled flow and heat transfer model
    Hu HaiYang
    Wang Qiang
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2010, 53 (10) : 2699 - 2707
  • [3] A numerical simulation on the infrared radiation of hot exhausting nozzles with a coupled flow and heat transfer model
    HU HaiYang WANG Qiang China Academy of Aerospace Aerodynamics Beijing China School of Jet Propulsion Beihang University Beijing China
    Science China(Technological Sciences), 2010, 53 (10) : 2699 - 2707
  • [4] A numerical simulation on the infrared radiation of hot exhausting nozzles with a coupled flow and heat transfer model
    HaiYang Hu
    Qiang Wang
    Science China Technological Sciences, 2010, 53 : 2699 - 2707
  • [5] A numerical simulation on the infrared radiation of hot exhausting nozzles with a coupled flow and heat transfer model
    HU HaiYang1 & WANG Qiang2 1 China Academy of Aerospace Aerodynamics
    2 School of Jet Propulsion
    Science China(Technological Sciences), 2010, (10) : 2699 - 2707
  • [6] CALCULATION OF HEAT-TRANSFER IN MODEL NOZZLES
    ZUBKOV, VG
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1991, (03): : 90 - 94
  • [7] Heat transfer prediction model of low-radiation diesel engine
    Liu Y.
    Liu Y.
    Wang L.
    Sun W.
    Ming P.
    Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University, 2021, 42 (07): : 1003 - 1008
  • [8] HEAT TRANSFER IN NOZZLES
    RAGSDALE, WC
    SMITH, JM
    CHEMICAL ENGINEERING SCIENCE, 1960, 11 (04) : 242 - 251
  • [9] Spectral radiation model for simulation of heat transfer in glass melts
    Lankhorst, Adriaan M.
    Faber, Anne Jans
    GLASS TECHNOLOGY-EUROPEAN JOURNAL OF GLASS SCIENCE AND TECHNOLOGY PART A, 2008, 49 (02): : 73 - 82
  • [10] Radiative heat transfer in film-cooled liquid rocket engine nozzles
    Badinand, T
    Fransson, TH
    JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2003, 17 (01) : 29 - 34