Fundamentals of the Theory and Design of a Gas Turbine Engine

Авторы: Zholdaspaev B.K., Beisebekova M.I., Kuljina G.S.

Издательство: EDP Hub (Идипи Хаб), Ай Пи Ар Медиа

This study aid covers design features and functional systems of various types of aviation gas turbine engines. The general theory, features of physical phenomena and working processes in the main nodes are also described: inlet guide unit (IGU), axial compressor (AC), combustion chamber (CC), turbine and output device (OD). Selection of materials used in aircraft engineering. The study aid is intended for students studying to become an aircraft mechanic when studying the disciplines “Aircraft engines” and “Aircraft technologies”.