期刊文献+

基于Lockheed模型的变密度多层绝热理论分析与实验 被引量:19

COMPUTATIONAL ANALYSIS OF VARIABLE DENSITY MULTILAYER INSULATION BASED ON THE LOCKHEED MODEL
下载PDF
导出
摘要 采用Lockheed模型,对变密度多层绝热的传热过程进行了理论分析,提出了最佳层密度的概念,重点讨论了层密度与边界温度关系、层密度区域划分、层密度配置和最佳层密度下热流密度的变化。分析得出较优的3区域层密度绝热结构和影响热流密度变化的热边界温度范围。同时通过实验验证,结果与计算的结果较好的吻合。 Lockheed model calculated density multilayer insulation heat transfer, proposed the concept of optimal layer density, and focus on the connection with layer density boundary temperature, layer density zoning, configuration layer density and optimal layer density under the change of the heat flux. Analysis of the superior region of the 3 layer density insulation struc- ture and main effects on heat flux density change in the thermal boundary temperature range. At the same time, experimental results and calculation results can be a good match.
出处 《真空与低温》 2013年第2期90-94,共5页 Vacuum and Cryogenics
关键词 变密度 多层绝热 层密度 Variable Density Muhilayer Insulation Layer Density
  • 相关文献

参考文献9

  • 1Hastings L J,Plachta D W,Salerno L, et al. An overview of NASA efforts on zero boil-off storage of cogenic propellants[ Jl. Cryogenics, 2002,41:833-839.
  • 2Hastings L J, Hedayat A, Brown T M. Analytical Modeling and Test Correlation of Variable Density Muhilayer Insulation for Cryo- genic Storage[ RI. NASA/TM-2004-213175, 2004.
  • 3Johnson W L. Thermal Performance of Cryogenic Muhilayer Insulation at Various Layer Spacing [ D ]. Florida: B. A.E. Auburn U- niversity, 2007.
  • 4Hastings L J,Tucker S P, Flachbart R H, et al. Marshall Space Flight Center In-Space Cryogenic Fluid Management Program O- verview[ C]. tilth AIAA/ASME/SAE/ASEE Joint propulsion conference & Exhibit. Arizona: 2005.
  • 5Martin J J, Hastings L. Hastings. Large-Scale Liquid Hydrogen Testing of Variable Density Multilayer Insulation with a Foam Sub- strate[ R]. NASA/TM-2001-211089, 2001.
  • 6Hedayat A,Brown T M,Hastings L J,et al. Variable density multilayer insulation for cryogenic storage [ C ]. 36th AIAA/ASME/ SAE/ASEE Joint propulsion conference & Exhibit. Huntsville: 2000.
  • 7Plachta D W, Christie R J,Jurns J M, et al. Passive ZBO storage of liquid hydrogen and liquid oxygen applied to space science mis- sion concepts[ J]. Cryogenics, 2006,46:89-97.
  • 8Lebar J F,Cady E C. The Advanced Cryogenic Evolved Stage(ACES)-A Low-Cost, Low-Risk Approach to Space Exploration Launch [ C ]. Space 2006. California: 2006.
  • 9朱浩唯,黄永华,许奕辉,吴静怡,李鹏.变密度多层绝热的理论分析[J].低温工程,2011(6):42-46. 被引量:18

二级参考文献8

  • 1魏蔚,汪荣顺.高真空多层绝热被的性能及其量热器的试验研究[J].低温与超导,2007,35(1):21-24. 被引量:13
  • 2Barth W, Lehmann W. Experimental investigations of superinsulation models equipped with carbon paper [ J ]. Cryogenics, 1988,28:317- 320.
  • 3Black I A. Basic investigation of multilayer insulation systems final report[ R]. NASA-54191,1964.
  • 4Jacob S,Kasthurirengan S,Karunanithi R. Investigations into the thermal performance of muhilayer insulation(300-77K) [ J]. Cryogenics, 1992,32(12) :1137-1153.
  • 5Tien C L,Cunnington G R. Radiation heat transfer in multilayer insulation having perforated shields[J]. Thermophysics and Spacecraft Thermal Control, 1974,35:65-74.
  • 6Hastings L J, Hedayat A, Brown T M. Analytical modeling and test correlation of variable density multilayer insulation for cryogenic storage [R]. NASA-213175,2004.
  • 7Martin J J, Hastings L. Large-scale liquid hydrogen testing of variable density multilayer insulation with a foam substrate [ R ]. NASA- 211089,2001.
  • 8孙培杰,吴静怡,张鹏,江明旒,徐烈.气体传热对多层绝热性能影响的试验研究[J].低温与超导,2008,36(11):6-12. 被引量:7

共引文献17

同被引文献189

引证文献19

二级引证文献44

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