摘要 : The article presents the results of numerical simulation of the boundary layer of air on a heated surface in the presence of weak acceleration. The numerical model consists of a system of Prandtl equations, describing dynamic and ... 展开
作者 | Sakhnov~ A. Yu. |
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作者单位 | |
期刊名称 | 《Thermophysics and Aeromechanics》 |
总页数 | 6 |
语种/中图分类号 | 英语 / O55 |
关键词 | boundary layer heat transfer laminarization velocity overshoot numerical modeling favorable pressure gradient BOUNDARY-LAYER TURBULENT TRANSITION FLOW |
馆藏号 | N2008EPST0009430 |