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

发散冷却控制烧蚀过程的数值研究
引用本文:谢远远,王建华.发散冷却控制烧蚀过程的数值研究[J].航空动力学报,2008,23(8):1381-1386.
作者姓名:谢远远  王建华
作者单位:中国科学技术大学 热科学与能源工程系, 合肥 230027
摘    要:用数值方法模拟了发散冷却控制结构烧蚀的瞬态过程,同时考虑了线烧蚀和体积烧蚀两种现象对多孔介质骨架高温表面的质量损失和冷却效果的影响,并讨论了高温主流携带的热流强度、冷却介质注入的初始速度和温度、及多孔材料骨架初始温度在控制烧蚀过程中的作用. 

关 键 词:线烧蚀    体积烧蚀    发散冷却    多孔介质
收稿时间:8/3/2007 3:08:00 PM
修稿时间:3/4/2008 10:26:16 AM

Numerical investigation of control ablation process with transpiration cooling
XIE Yuan-yuan and WANG Jian-hua.Numerical investigation of control ablation process with transpiration cooling[J].Journal of Aerospace Power,2008,23(8):1381-1386.
Authors:XIE Yuan-yuan and WANG Jian-hua
Institution:Department of Thermal Science and Energy Engineering, University of Science and Technology of China, Hefei 230027, China
Abstract:A numerical method was developed to simulate the transient control ablation process by transpiration cooling.The influence of surface ablation and charring of thermal protective structure on cooling performance and the mass losses due to the ablation and charring was considered.In order to exactly predict the performance of the control ablation and cooling process,the influences of heat flux intensity,coolant injection velocity,initial temperatures of porous matrix and coolant on the cooling effect were discussed.
Keywords:surface ablation  charring  transpiration cooling  porous matrix
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