Reynolds Analogy in the Boundary layer with ex-ternal impact
The paper considers various methods of impacts on the boundary layers that allow controlling the Reynolds analogy factor. The results of studying the effect of heat transfer enhancement, imposition of large-scale vortex structures, and longitudinal pressure gradient are described. Dimples of various shapes and arrays are considered as heat transfer enhancement. Imposition of vortex structures is studied on the wall in the cylinder wake. An adverse pressure gradient is studied in compressible and incompressible nonequilibrium boundary layers, while a favorable pressure gradient is studied in a supersonic nozzle. The results show that in the flows considered, the Reynolds analogy factor can exceed the values for a zero-pressure gradient boundary layer.
В работе рассмотрены различные способы воздействия на пограничные слои, позволяющие управлять фактором аналогии Рейнольдса. Описаны результаты исследования влияния интенсификаторов теплообмена, наложения крупномасштабных вихревых структур, а также продольного градиента давления. В качестве интенсификаторов теплообмена рассмотрены лунки различной формы и компоновки. Наложение вихревых структур исследовано на стенке в следе цилиндра. Неблагоприятный градиент давления исследован в сжимаемом и несжимаемом неравновесном пограничном слое, в то время как благоприятный градиент давления - в сверхзвуковом сопле. Полученные результаты показывают, что в рассмотренных течениях фактор аналогии Рейнольдса может превышать значения для безградиентного пограничного слоя.
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