Calculation of the base flow behind the rounded trailing edge of a two-dimensional body separating two supersonic streams

A method of calculating the base pressure and the coordinates of the separation points on the curved surface of the trailing edge of a two-dimensional body separating two supersonic streams, taking into account the local overexpansion effect, has been developed.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 170–173, November–December, 1991.