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高超声速边界层流动转捩研究
Alternative TitleStability and Transition of Hypersonic Boundary Layer Flow
刘嘉; 雷麦芳; 姚文秀; 王发民
Source Publication计算物理
2004-01-25
Volume21Issue:1Pages:61-67
ISSN1001-246X
Abstract针对高超声速飞行器前体预压缩性所需求的气动构型,开展了具有一级压缩效果的压缩面边界层的流动稳定性分析.采用有限体积法数值求解NS方程组得到基本流场,应用当地局部平行流假设和线性稳定性理论求解了扰动波参数的特征值问题.分析了来流马赫数M∞=6情况下二维扰动波的演化规律,并进一步关联扰动的空间放大率,结合EN方法进行了转捩预测.
Keyword高超声速流动 稳定性分析 转捩
Indexed ByCSCD
Language中文
CSCD IDCSCD:1565822
Citation statistics
Cited Times:3[CSCD]   [CSCD Record]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/42200
Collection力学所知识产出(1956-2008)
Corresponding Author刘嘉
Recommended Citation
GB/T 7714
刘嘉,雷麦芳,姚文秀,等. 高超声速边界层流动转捩研究[J]. 计算物理,2004,21(1):61-67
APA 刘嘉,雷麦芳,姚文秀,&王发民.(2004).高超声速边界层流动转捩研究.计算物理,21(1),61-67.
MLA 刘嘉,et al."高超声速边界层流动转捩研究".计算物理 21.1(2004):61-67.
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