Approximate solution method for the problem of flowing over a body of revolution with concave generating line

Definition and solution of the problem of flowing around the bodies of revolution with concave generators, are analysed. Solution of a set of partial differential equations describing the supersonic flow of ideal gas, is presented in the form of power series with variable coefficients. Integration of this set of equations is reduced to sequential integration of a systems of ordinary differential equations. The results of calculated pressure distribution over the surface of a weakly concave body agree satisfactorily with the experimental results for supersonic velocities.