CALCULATION OF TRANSONIC FLOW PAST THE AFTER-PART OF A PLANE OR AXISYMMETRICAL BODY

On the basis of a modified Godunov finite-difference scheme, a method is given for calculating the transonic flow of an ideal gas past the after-part of a plane or axisymmetric elongated body with large angles of inclination and breaks in the generators. Differences schemes adapted to the flow singularities are used, and a new version of the scheme is realized. Relations for the transonic flow remote from the body are obtained in the linear approximation.