Theory of Compressors and Turbines for Aviation Gas Turbine Engines. Textbook

The basics of the theory, methods for choosing the main parameters and thermogazodynamic calculations of the shovel machines (axial and centrifugal compressors, axial and centroting turbines) of aviation gas turbine engines are presented. Materials related to the characteristics of the characteristics of compressors and turbines in the calculated and non -calculated modes of their work are set out. The main equations and spatial models of the fluid flow in the canal machines are considered.
For students of higher educational institutions studying in the areas of preparation of undergraduate and graduate engines of aircraft ", a specialist" Design of aviation engines and power plants", as well as in adjacent areas of training and specialties