Calculation of three-dimensional supersonic steady vortex flows by the method of characteristics

Abstract

The investigation is concerned with three-dimensional supersonic steady gas flows. The aim to be attained is to develop numeric methods to solve the problems of supersonic gas dynamics. A problem of shaping three-dimensional supersonic channels with a central body has been solved. An effective algorithm of calculation of supersonic vortex flows has been developed. A program package for calculation of supersonic vortex flows, calculation of points being on a rigid boundary or impact wave and for channers shaping has been developedAvailable from VNTIC / VNTIC - Scientific & Technical Information Centre of RussiaSIGLERURussian Federatio