Supercritical regimes of hypersonic flow past a planar yawed delta wing

Hypersonic viscous perfect gas flow past a planar delta wing in the viscous-inviscid interaction regime is considered. The effect of the yaw angle on the parameters of the laminar boundary layer on the cold wing and the formation of subcritical and supercritical flow regions is studied.Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 4, pp. 151–158, July–August, 1995.