IMECH-IR  > 力学所知识产出(1956-2008)
壁温对高超音速钝锥边界层稳定性的影响
梁贤; 李新亮; 傅德薰; 马延文
Source Publication第五届全国青年计算物理学术交流会论文摘要.中国核学会,2008,p.83-84
2008
Pages83-84
Conference Name第五届全国青年计算物理学术交流会
Conference Date2008
Conference Place山东青岛
Abstract高超音速边界层转捩预测是高超音速飞行器气动力及气动热分析的关键因素。作为高速飞行器的典型头部外形,钝锥边界层流动的转捩机理和转捩预测具有重要的实际意义,是目前研究高速飞行器气动力和气动热特征的重要课题。由于人们对影响转捩的物理机理并不是十分清楚,因此,目前对于高超音速边界层的转捩的预测多采用半经验的方法,很多经验参数还依赖实验给定。
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/34392
Collection力学所知识产出(1956-2008)
Corresponding Author梁贤
Recommended Citation
GB/T 7714
梁贤,李新亮,傅德薰,等. 壁温对高超音速钝锥边界层稳定性的影响[C]:中国核学会,2008:83-84.
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