Mathematical model of the technological process of testing the gas generator of a bypass turbojet engine

Abstract

A mathematical model for testing a gas generator of a bypass turbojet engine, which is used to increase the level of test automation, has been formed and presented. The mathematical model describes the technological process of testing the gas generator of a bypass turbojet engine with the simulation of the required input thermogasdynamic parameters. It is shown that the results of calculations using the proposed model are in good agreement with the experimental data of the operation of a specialized test complex for testing the gas generator of a bypass turbojet engine.