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The aim of this article was the development of the gas-dynamic models allowing to calculate the working
processes of the gas turbine engine (GTE) in the compressor, in the combustion chamber and in the turbine at the same
time. The possibilities of software systems for complex engine workflow modeling are specified. The advantages and
disadvantages of the presented methods are specified. The results of complex GTE simulation in a single software product
are presented. It is shown that the results of a complex gas dynamic modeling are in a good agreement with the calculation
results obtained using a calibrated one-dimensional thermodynamic model.