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

发散冷却最小冷却介质注射量的数值研究
引用本文:时骏祥,王建华.发散冷却最小冷却介质注射量的数值研究[J].航空动力学报,2007,22(2):222-227.
作者姓名:时骏祥  王建华
作者单位:中国科学技术大学,热科学及与能源工程系,合肥,230027
基金项目:国家自然科学基金 , 安徽省教育厅自然科学基金重点项目 , 教育部留学回国人员科研启动基金
摘    要:充分发挥材料本身的抗高温能力,以最小的冷却介质注射量,确保推进器不被烧蚀是发散冷却系统的设计目标.本文用一维可压缩、非稳态、局部非热平衡模型,数值研究了瞬态冷却过程及最小冷却介质注射量的依赖参数.数值研究表明:研究瞬态的冷却过程十分重要, 因为尽管当冷却过程达到稳态以后热端温度在烧蚀点以下,但在进入稳态之前可能已经发生烧蚀;多孔介质骨架材料的初始温度越高、特征尺寸越大,冷却介质需要量越大;在仅考虑冷却效果的前提下,孔隙率越大,冷却介质需要量越大;相反,骨架材料导热系数越高,冷却介质需要量越小.

关 键 词:航空、航天推进系统  发散冷却  冷却介质  最小注射量  发散冷却  最小  冷却介质  注射量  数值研究  transpiration  cooling  rate  injection  coolant  minimum  导热系数  孔隙率  前提  冷却效果  需要量  特征尺寸  初始温度  骨架材料  多孔介质  发生
文章编号:1000-8055(2007)02-0222-06
收稿时间:2006/2/16 0:00:00
修稿时间:2006年2月16日

A numerical investigation of the minimum coolant injection rate for transpiration cooling
SHI Jun-xiang and WANG Jian-hua.A numerical investigation of the minimum coolant injection rate for transpiration cooling[J].Journal of Aerospace Power,2007,22(2):222-227.
Authors:SHI Jun-xiang and WANG Jian-hua
Institution:Department of Thermal Science and Energy Engineering, University of Science and Technology of China, Hefei 230027, China;Department of Thermal Science and Energy Engineering, University of Science and Technology of China, Hefei 230027, China
Abstract:An advanced design of transpiration cooling system is not only to ensure thermal protection of propulsion system from ablation,but it also should utilize the full temperature potential of porous matrix.A numerical investigation of transient processes of transpiration cooling and the control parameters of the lowest limit of the coolant mass flow rate is conducted with the help of a compressible, unsteady and local non-thermal equilibrium model.The numerical investigation presents that it is important to study transient cooling process,because the porous matrix could be ablated before the cooling process reaches a steady state,though the steady temperature may be lower than the melting point.A higher initial temperature and a larger characteristic size of the porous matrix will result in an increase in the minimum coolant injection rate to prevent ablation of the porous matrix.From the view point of cooling effect,a higher porosity corresponds to a larger coolant mass flow rate.Contrarily,a higher thermal conductivity of the porous matrix corresponds to a lower demand for the minimum coolant flow rate.
Keywords:aerospace propulsion system  transpiration cooling  coolant  minimum injection rate
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
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