俄罗斯空气动力研究所中心学报
每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
HEAT FLUX TO THE CYLINDER SURFACE AT THE THREE-DIMENSIONAL PERTURBATIONS OF SUPERSONIC FLOW
卷 44,
册 2, 2013,
pp. 185-204
DOI: 10.1615/TsAGISciJ.2013008127
摘要
Three-dimensional flow in the shock layer at a supersonic flow over the cylinder frontal surface under imposed small space-periodic perturbations was studied in this work. On the basis of the numerical solution of the unsteady three-dimensional Navier-Stokes equations it was demonstrated that the small imposed perturbations of the incoming flow in the transversal coordinate result in the distortion of the shock wave front, in the generation of the significantly three-dimensional flow in the region of the shock wave, and in the formation of large heat flux perturbations on the surface.
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