Optimization of operating process parameters and choice of schemes of small-sized two-circuit turbojet engines for various aircraft

Abstract

The article poses a problem and defines the initial data for optimization of small-size by-pass turbojet engines. The results of optimization of the parameters of the working process and the choice of rational schemes of small-sized by-pass turbojet engines for light, administrative and regional civil aircraft are presented. An assessment of the reliability of the developed method was carried out, as well as conclusions on the work were written and a way for the further development of the considered topic was outlined.