IMECH-IR  > 高温气体动力学国家重点实验室
不同流态对高超声速飞行器热流的影响
雷麦芳; 李维东; 王发民
Source Publication高温气体动力学研究进展
2012
Pages255-260
Conference NameLHD2012夏季学术研讨会
Conference Date2012
Conference Place吉林延吉
Abstract近空间高超声速巡航飞行,面临高升阻比复杂布局和长时间中低热流的气动热环境。飞行器周围流场中激波边界层干扰等复杂的流动现象,以及层流、转捩区和完全发展湍流等不同流态对气动热特性的影响,是一个很重要的工程科学问题。本文探讨了不同流态对气动加热的影响规律,建立了不同流态热流计算模型和数值求解方法。通过典型布局气动热实验结果的对比,说明模型是合理的。
Keyword气动加热 湍流模型 高超声速
DepartmentLHD高超声速空气动力学
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/48009
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
雷麦芳,李维东,王发民. 不同流态对高超声速飞行器热流的影响[C]高温气体动力学研究进展,2012:255-260.
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