S. S. Remchukov, I. V. Osipov, Maxim Danilov, I. S. Ptitsyn, R. N. Lebedinskii, Evgeny Polyakov
Abstract
Abstract A small-sized turbofan jet engine demonstrator with a thrust up to 2000 N was developed. The project was implemented using a concept of development of gas turbine engine family based on a unified core engine.
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Abstract A small-sized turbofan jet engine demonstrator with a thrust up to 2000 N was developed. The project was implemented using a concept of development of gas turbine engine family based on a unified core engine.
Key concepts: Turbofan, Jet engine, Thrust, Gas turbines, Core (optical fiber), Automotive engineering, Aerospace engineering, Turbine