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Энергетическая ГТУ малой мощности на базе авиационного двигателя

In this final qualifying work, the conversion of the AI-24 turboprop aviation gas turbine engine with a capacity of 2 MW was performed into a ground-based GTU with a capacity of 4 MW. The thesis includes an introduction, three chapters and a conclusion. The work includes thermal calculations of the GTD cycle; gas dynamic calculations of the compressor;
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