IMECH-IR  > 高温气体动力学国家重点实验室
飞行高度对高超声速模型飞行器气动性能影响的计算分析
朱辉玉; 杨弼杰; 孙泉华; 樊菁
Source Publication第四届高超声速科技学术会议会议日程及摘要集
2011
Pages10
Conference Name第四届高超声速科技学术会议
Conference Date2011
Conference Place中国海南三亚
Abstract<正>高超声速飞行器飞行时具有激波-激波、激波-边界层、以及激波-漩涡相互作用等复杂的流动物理,正确预测高超声速飞行器的气动性能具有很大的挑战性。而层流条件下的数值预测能力应该是真实环境计算评估的基础。本文针对高速飞行器在近空间大范围的飞行条件,对二维外形的模型飞行器在马赫数6飞行时的气动性能作了层流计算。计算外形采用吸气式气动布局,能够很好地包含高
Keyword高超声速流动 计算网格 吸气式布局 层流
DepartmentLHD微尺度和非平衡流动
Funding Organization中国力学学会、中国科学院高超声速科技中心、中国科学院力学研究所、高温气体动力学国家重点实验室
URL查看原文
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/45310
Collection高温气体动力学国家重点实验室
Corresponding Author朱辉玉
Recommended Citation
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朱辉玉,杨弼杰,孙泉华,等. 飞行高度对高超声速模型飞行器气动性能影响的计算分析[C]第四届高超声速科技学术会议会议日程及摘要集,2011:10.
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