Abstract:
A numerical-analytical method is developed for determining the shape of a streamlined with jet blowing axisymmetric body from a given velocity distribution along its meridional section. Numerical result examples are given. Forces, which are influence on axisymmetric body, are calculated. Comparisons of aerodynamic characteristics for bodies with different location of annular channel are carried out.
Key words:inverse boundary value problem of aerohydrodynamics, ideal incompressible fluid, axysim-metric body, annular channel, jet, iterative process.