首页 | 本学科首页   官方微博 | 高级检索  
     检索      

层板发汗冷却推力室传热分析
引用本文: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(1):17-21,39.
作者姓名:黄春桃  孙冰
作者单位:北京航空航天大学宇航学院,北京,100191
摘    要:对于采用层板发汗冷却的推力室,为了最大限度地减少冷却剂流量,理想情况是,应根据不同轴向位置的受热情况来分配冷却剂流量,以使各处的壁面温度都控制在材料的许用温度内.本文运用有限体积法,对层板发汗冷却推力室内的燃气流动和壁面内的传热进行了数值模拟,同时通过调节冷却剂吹风比,使各处的壁面温度都控制在材料的许用温度之内.为综合...

关 键 词:层板推力室  发汗冷却  耦合传热  数值模拟

Heat transfer analysis of platelet transpiration cooling thrust chamber
HUANG Chun-tao,SUN Bing.Heat transfer analysis of platelet transpiration cooling thrust chamber[J].Journal of Rocket Propulsion,2011,37(1):17-21,39.
Authors:HUANG Chun-tao  SUN Bing
Institution:(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)
Abstract:For a platelet transpiration cooled thrust chamber,in order to achieve the maximum reduction of the coolant flow rate,the ideal means is to distribute the coolant according to different axial heating positions to keep overall wall temperature under material permissible limit.The numerical simulation for the internal gas flow and wall heat transfer in a platelet transpiration cooled thrust chamber were performed by using finite volume method.The two aspects of transpiration cooling,the heat transfer in the wall and the obstructing effect of blowing ratio on the surface temperature,were solved in a coupled solution to consider the transpiration cooling effect synthetically.The numerical results show that blowing ratio increases with the decrease of the wall temperature.
Keywords:platelet thrust chamber  transpiration cooling  coupled heat transfer  numerical simulation
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号