PDF下载 分享
[1]张峰,刘伟强.层板发汗冷却在液体火箭发动机中的应用与发展综述[J].火箭推进,2007,33(06):43-48.
 Zhang Feng,Liu Weiqiang.Application and development of platelet transpiration cooling technology in LRE[J].Journal of Rocket Propulsion,2007,33(06):43-48.
点击复制

层板发汗冷却在液体火箭发动机中的应用与发展综述

相似文献/References:

[1]高翔宇,孙纪国,田 原.推力室多孔面板氢发汗冷却传热分析[J].火箭推进,2012,38(05):13.
 GAO Xiang-yu,SUN Ji-guo,TIAN Yuan.Numerical analysis of H2 transpiration cooling for thrust chamber porous plate[J].Journal of Rocket Propulsion,2012,38(06):13.
[2]黄春桃,孙 冰.层板发汗冷却推力室传热分析[J].火箭推进,2011,37(01):17.
 HUANG Chun-tao,SUN Bing.Heat transfer analysis of platelet transpiration cooling thrust chamber[J].Journal of Rocket Propulsion,2011,37(06):17.
[3]高翔宇,孙纪国.推力室多孔面板发汗冷却试验研究[J].火箭推进,2011,37(05):9.
 GAO Xiang-yu,SUN Ji-guo.Experimental study on porous plate transpiration cooling of thrust chamber[J].Journal of Rocket Propulsion,2011,37(06):9.
[4]雷娟萍,林革.小型化高床载过氧化氢整体式催化剂床研究[J].火箭推进,2008,34(04):12.
 Lei Juanping,Lin Ge.Small high-flux hydrogen peroxide integrated catalyst bed[J].Journal of Rocket Propulsion,2008,34(06):12.

更新日期/Last Update: 1900-01-01