IMECH-IR  > 高温气体动力学国家重点实验室
高超声速飞行器内外流耦合数值模拟方法
王发民; 张陈安; 李维东; 雷麦芳
Source Publication高温气体动力学研究进展
2012
Pages181-187
Conference NameLHD2012夏季学术研讨会
Conference Date2012
Conference Place吉林延吉
Abstract针对以冲压发动机为动力的高超声速飞行器前体预压缩特性、燃烧室热力学特性,以及高温化学反应物理特性等工程科学问题,设计了原理上总压损失较小的超燃燃烧室,进行了乘波体/超燃冲压发动机一体化设计。建立了碳氢燃料超燃燃烧室化学反应模型。研究了前体预压缩特性和对进气道的影响规律;模拟了超燃冲压发动机内通道一体化化学反应和流动特性耦合现象。
Keyword高温非平衡化学反应 乘波布局 内外流耦合计算
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/311007/47997
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
王发民,张陈安,李维东,等. 高超声速飞行器内外流耦合数值模拟方法[C]高温气体动力学研究进展,2012:181-187.
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