中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Thermal Protection Efficiency of Forward-facing Cavity and Opposing Jet Combinational Configuration

文献类型:期刊论文

作者Haibo Lu; Weiqiang Liu
刊名JOURNAL OF THERMAL SCIENCE
出版日期2012
卷号21期号:4页码:342,347
关键词Thermal Protection Forward-facing Cavity Opposing Jet Nose-tip Aerodynamic Heating
英文摘要To deal with the thermal protection of high speed vehicle, the cooling efficiency of a combinatorial thermal protection configuration which is composed of the forward-facing cavity and opposing jet is investigated. The numerical simulation result is validated by experiment and the flow field parameters, aerodynamic force and heat flux distribution are obtained. The detailed numerical simulation results show that this kind of combinatorial thermal protection configuration has an excellent effect on cooling the surface of the nose-tip. By adding of the opposing jet with a small total pressure, it can avoid the disadvantage to the control performance of the aircraft which is caused by the cavity oscillating flow. And the low stagnation pressure is propitious to simplify the opposing jet system. The location of the recirculation region has a significant impact of the aerodynamic heating. The heat flux along outer body surface of the nose-tip does not increase with the stagnation pressure of opposing jet decreases monotonically.
公开日期2013-01-07
源URL[http://ir.etp.ac.cn/handle/311046/51785]  
专题工程热物理研究所_Journal of Thermal Science
推荐引用方式
GB/T 7714
Haibo Lu,Weiqiang Liu. Thermal Protection Efficiency of Forward-facing Cavity and Opposing Jet Combinational Configuration[J]. JOURNAL OF THERMAL SCIENCE,2012,21(4):342,347.
APA Haibo Lu,&Weiqiang Liu.(2012).Thermal Protection Efficiency of Forward-facing Cavity and Opposing Jet Combinational Configuration.JOURNAL OF THERMAL SCIENCE,21(4),342,347.
MLA Haibo Lu,et al."Thermal Protection Efficiency of Forward-facing Cavity and Opposing Jet Combinational Configuration".JOURNAL OF THERMAL SCIENCE 21.4(2012):342,347.

入库方式: OAI收割

来源:工程热物理研究所

浏览0
下载0
收藏0
其他版本

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。