Konstantinov V. The analysis and optimization of physical processes for aerodynamic perfection of turbomachinery rows.

The dissertation is devoted to design frontier topics that are connected with the structurization, modelling and optimization of the physical processes in complicate technical systems (as the latter there is treated a class of turbomachinary rows). The system mathematical model and generalized algorithm for solving the problems of an analysis and optimization of physical processes in blade-to-blade channels of turbomachinery rows are considered. The individual mathematical models, technique of an analysis and calculation of nearwall viscous flows are developed. The technique of morphological synthesis for ra-tional 3D representation of turbomachinery rows on the basis of complex use of control flow separation systems is developed. The technology and CAE - system for its information support, synthesis of rational 3D representa-tion of axial flow compressor rows is developed, the high efficiency of which is confirmed while solving practical problems.