Development of an Advanced Small-Sized Turbofan Engine Based on a Core Engine.
| Autor: | Remchukov, S. S., Osipov, I. V., Danilov, M. A., Ptitsyn, I. S., Lebedinskii, R. N., Polyakov, E. A. |
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| Zdroj: | Russian Aeronautics; Jan2023, Vol. 66 Issue 1, p79-86, 8p |
| Abstrakt: | 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. [ABSTRACT FROM AUTHOR] |
| Databáze: | Complementary Index |
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