IMECH-IR  > 高温气体动力学国家重点实验室
高超声速飞行器摩阻预估
陈文龙; 张陈安; 韩汉桥; 王发民
Source Publication高温气体动力学研究进展
2011
Pages307-312
Conference NameLHD2011夏季学术研讨会
Conference Date2011
Conference Place内蒙赤峰
Abstract表面摩阻是影响高超声速飞行器性能的重要因素,在高超声速飞行情况下摩擦阻力在总阻力中占有很重要的一部分。本文应用CFD 技术来研究摩擦阻力在不同乘波体飞行器在不同飞行条件下的壁面摩擦阻力。计算结果表明,在高超声速高空的情况下,摩阻已经达到和波阻一个量级。摩阻的准确预估是飞行器气动力与气动热重要的一部分。
Keyword高超声速飞行器 摩阻 Cfd 技术
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/311007/47953
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
陈文龙,张陈安,韩汉桥,等. 高超声速飞行器摩阻预估[C]高温气体动力学研究进展,2011:307-312.
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