Abstract: An approach to creating compact and miniature infra- and low-frequency vibration isolation systems based on layered composite elastic elements with adjustable negative and quasi-zero stiffness is presented. New problems of modeling the given parameters of the stiffness and bearing capacity of elements of certain geometry under combined loading have been solved by varying the structure, elastic properties, and arrangement of layers and controlling the local mobility of the binder. The correctness of the approach is based on the results of experimental design and research of system models. This approach can qualitatively change the solution of a number of critical problems in vibroacoustics of aviation and other advanced engineering

Cite: Karpov E.V. , Larichkin A.Y. , Goverdovskiy V.N. , Brovkina Y.I. , Prokhorov A.N.
Prestressed Multilayer Structures from Polymer Composites for Vibration and Noise Control of Aircraft
Doklady Physics. 2023. Т.68. №8. С.60-66. DOI: 10.1134/S1028335823080037 WOS Scopus РИНЦ OpenAlex

Original: Карпов Е.В. , Ларичкин А.Ю. , Говердовский В. , Бровкина (Николаева) Ю.И. , Прохоров А.Н.
ПРЕДНАПРЯЖЕННЫЕ МНОГОСЛОЙНЫЕ КОНСТРУКЦИИ ИЗ ПОЛИМЕРНЫХ КОМПОЗИТОВ ДЛЯ РЕШЕНИЯ ЗАДАЧ ВИБРОАКУСТИКИ ЛЕТАТЕЛЬНЫХ АППАРАТОВ
Доклады Российской академии наук. Физика, технические науки.. 2023. Т.511. №1. С.60-66. DOI: 10.31857/S2686740023040053 РИНЦ OpenAlex

Dates:

Submitted:	Feb 6, 2023
Accepted:	May 4, 2023
Published print:	Feb 15, 2024

Identifiers:

Web of science:	WOS:001162761300002
Scopus:	2-s2.0-85185409881
Elibrary:	60053544
OpenAlex:	W4391858443

Citing: Пока нет цитирований

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