Abstract:
To date, the turbojet dual-circuit engine (turbojet) is the most common air-jet aircraft engine due to low fuel consumption and a number of other advantages. The purpose of this work is to develop a software package for calculating the parameters of the flow part of the turbojet with an intuitive and user-friendly modern interface that allows further expansion of the functionality due to the modular architecture. The developed software package is allowed to raise the process of designing the flow part of the turbojet to a higher level, thereby reducing not only the time of its development, but also the costs.
Keywords:turbinectomy turbofan engine, design, development of software.