IMECH-IR  > 高温气体动力学国家重点实验室
高超声速流线追踪进气道基准流场设计
岳连捷; 肖雅彬; 陈立红; 张新宇
Source Publication第二届高超声速科技学术会议会议日程及摘要集.中国力学学会,2009,p.22
2009-11-02
Pages22
Conference Name第二届高超声速科技学术会议
Conference Date2009-11-02
Conference Place中国安徽黄山
Abstract 本文发展了一种流线追踪进气道基准流场设计方法。截短Busemann进气道由于其长度限制,使得对称轴附近激波弯曲程度严重,造成较大的总压损失。本文采用ICFA来使激波变直,通过优化由样条曲线构成的下游流动来获得最大总压恢复。尽管激波弯曲现象依然存在,但已经被限制在靠近对称轴的很小的区域内。与同样长度和收缩比的截短Busemann内锥流相比,本文设计的流动具有更高的总压恢复。
Keyword高超声速 流线追踪进气道 基准流场
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/43121
Collection高温气体动力学国家重点实验室
Corresponding Author岳连捷
Recommended Citation
GB/T 7714
岳连捷,肖雅彬,陈立红,等. 高超声速流线追踪进气道基准流场设计[C]:中国力学学会,2009:22.
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