V-wing supersonic flow regimes with viscous interaction modelingстатья
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Дата последнего поиска статьи во внешних источниках: 28 мая 2015 г.
Аннотация:Possible regimes of supersonic flow around a V-wing of given geometry are fully analyzed on a freestream Mach number/angle of attack parameter range. A previously developed boundary layer displacement thickness model for conical angular configurations is used. The change in the relative arrangement of the characteristic curves and regimes of flow around a V-wing representing the undersurface of an equivalent waverider with given specific volume and lift coefficient, which accompanies a decrease in the aperture angle, is studied.