## A method for computing supersonic flow around blunt bodies, accompanied by a detached shock wave |

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_ x _ accuracy algorithm analytical character analytical continuation analytical curve analytical functions approximate solution approximating system 2.8 approximating system 3.12 axis of symmetry blunt body bounded second derivative Cauchy problem Chebyshev polynomial class of analytical class of functions complex region conditions 3.8 conditions of symmetry consider const desired solution detached shock wave determine the solution difference approach difference method elliptical region error in approximation errors in rounding FLOW AROUND BLUNT formulation gas dynamics hodograph plane increase of errors initial line iteration process Lagrange interpolation polynomials Lagrange polynomials Laplace equation limiting curve number of intervals number of nodes number of rays numerical solution ordinary differential equations parameters perfect gas physical plane precise solution prob problem of supersonic region AGTFE region of convergence region of influence segment solu solution J>(x solutions of equation sonic line subsonic system of ordinary Taking into account tion upper half-plane variables wave equation