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СВОБОДНЫЕ КОЛЕБАНИЯ ЛОПАТОК ОСЕВОГО КОМПРЕССОРА ГАЗОТУРБИННОГО ДВИГАТЕЛЯ

Published in Aerospace technic and technology • Aug 31, 2020
NobleIDNI0P94W28R37S24
Authors:
Mykhaylo Tkach
,
Сергей Александрович Моргун
,
Юрий Григорьевич Золотой

Abstract

The required level of reliability of modern gas turbine engines cannot be achieved without ensuring the vibrational strength of the compressor blades. One of the tasks of ensuring vibrational strength is to determine the frequency spectrum of free vibrations, as well as the arising forms of vibratio...

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