Knowledge Management System of Institue of Mechanics, CAS
Chemical Nonequilibrium Effects on Flow Field for Reusable Launch Vehicles | |
Ma H(马辉)![]() ![]() ![]() | |
Source Publication | Shock Waves |
2004-11-22 | |
Pages | 155-160 |
Conference Name | 24th International Symposium on Shock Waves, JUL 11-16, 2004 Beijing, PEOPLES R CHINA |
Conference Date | JUL 11-16, 2004 |
Conference Place | Beijing, PEOPLES R CHINA |
Abstract | High temperature chemical non-equilibrium phenomena have a great effect on the flow field around a reentry vehicle. A set of three dimensional Navier-Stokes equations have been solved by implicit finite volume NND scheme. Both ideal gas viscous flow and chemical non-equilibrium flow are calculated for a spherical-cone at a small angle of attack. The results of the two flows have been compared and the effect of chemical non-equilibrium has been analyzed. The effect of wall material's properties, such as catalysis and radiation were studied. The results are in good agreement with the referenced paper. |
WOS ID | WOS:000231243300020 |
Indexed By | CPCI-S |
Language | 英语 |
Citation statistics | |
Document Type | 会议论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/13745 |
Collection | 力学所知识产出(1956-2008) |
Corresponding Author | Wang FM(王发民) |
Recommended Citation GB/T 7714 | Ma H,Zhao L,Wang FM,et al. Chemical Nonequilibrium Effects on Flow Field for Reusable Launch Vehicles[C]Shock Waves,2004:155-160. |
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