Study of dynamics and rigidity of multifunctional coating of protective element of aircraft

Study of dynamics and rigidity of multifunctional coating of protective element of aircraft

In this work using a finite element study the author has numerically solved the problem of the dynamic behavior of a multifunctional coating of an aircraft protective element. The researcher conducted the simulation using the Femap with NX Nastran software package, The result of the modal analysis...

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Bibliographic Details
Main Author: A. V. Kupryashov
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2021-03-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
Subjects:
finite element method
stiffness
numerical simulation
vibration frequency
modal analysis
protective coating
Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2021/%D0%A2.%205,%20%E2%84%96%201%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/86-94%20%D0%9A%D1%83%D0%BF%D1%80%D1%8F%D1%88%D0%BE%D0%B2%20%D0%90.%20%D0%92..pdf
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