doi: 10.18698/2309-3684-2020-4-2743
For mathematical modeling of subsonic separation flow around axisymmetric bodies with a bottom section, a technique with a partial implementation of the concept of visco–inviscid interaction was used. A flow scheme with an equivalence semi-infinite surface was used. Numerical simulations were carried out according to the algorithms of the method using the method of discrete vortices and approximation by smoothing cubic splines. Data on the influence of the shape of the tail section of an equivalent surface on the velocity and pressure distribution during axisymmetric flow around bodies with a bottom section are presented. The proposed recommendations make it possible to apply this technique more universally.
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