NUMERICAL ANALYSIS OF TWO-DIMENSIONAL PROBLEM OF SUPERSONIC SHOCK WAVE INTERACTION WITH A BOUNDARY LAYER
Journal Title: Інформаційні системи, механіка та керування - Year 2015, Vol 0, Issue 12
Abstract
The results of numeric modeling of the nature of supersonic turbulent flows interaction in the field of inclined from the windward side plane of the step for thecanting angle β = 8, 25, 90° and Mach numbers M∞ = 2,9, 2,94. The Navier-Stokes equations averaged by Reynolds with the usage of turbulent model were used as a mathematical model k-ω SST for viscous compressed environment. Comparative analysis of the pressure distribution and surface friction with gained experimental data was held.
Authors and Affiliations
Анатолій Юрійович Педченко, Євген Миколайович Панов,, Антон Янович Карвацький,, Сергій Володимирович , Лелека, Тарас Валерійович Лазарєв
Keywords
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