Abstract
One approach to designing turbomachine blades is to use the theory of inverse boundary-value problems of aerohydrodynamics. The basis of the method for solving the inverse problem for a profile lattice located on an axisymmetric stream surface in a layer of variable thickness is the solution of the problem for a flat lattice. In this paper, we consider a number of issues arising in the numerical implementation of the solution of this problem for dense lattices, and we propose methods for solving them and thereby increase the accuracy of numerical calculations.
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