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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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"
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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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author A. V. Kupryashov
author_facet A. V. Kupryashov
author_sort A. V. Kupryashov
collection DOAJ
description 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 is the values and patterns of natural and secondary vibration modes of the multifunctional coating of the protective element of the aircraft using a special module the author has determined the distribution of effective modal masses in tabular form, Also, as a result of calculations, the author of the article obtained the value of the structural rigidity of the protective coating, The results presented in this work allow us to analyze the behavior of protective systems and structural elements of an aircraft with a multifunctional coating applied to the outer surface in real operating conditions, The design team can use the research results of this article in order to increase the efficiency of the development of a new structures and structures of a composite coating for multifunctional purposes, protective elements and materials for space technology
format Article
id doaj-art-d7e3bd439d844e89998f43532f08aa83
institution Kabale University
issn 2588-0373
2587-764X
language English
publishDate 2021-03-01
publisher Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
record_format Article
series Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
spelling doaj-art-d7e3bd439d844e89998f43532f08aa832025-02-02T14:56:19ZengOmsk State Technical University, Federal State Autonomous Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2021-03-0151869410.25206/2588-0373-2021-5-1-86-94Study of dynamics and rigidity of multifunctional coating of protective element of aircraftA. V. Kupryashov0https://orcid.org/0000-0003-1296-4942Reshetnev Siberian State University of Science and TechnologyIn 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 is the values and patterns of natural and secondary vibration modes of the multifunctional coating of the protective element of the aircraft using a special module the author has determined the distribution of effective modal masses in tabular form, Also, as a result of calculations, the author of the article obtained the value of the structural rigidity of the protective coating, The results presented in this work allow us to analyze the behavior of protective systems and structural elements of an aircraft with a multifunctional coating applied to the outer surface in real operating conditions, The design team can use the research results of this article in order to increase the efficiency of the development of a new structures and structures of a composite coating for multifunctional purposes, protective elements and materials for space technologyhttps://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..pdffinite element methodstiffnessnumerical simulationvibration frequencymodal analysisprotective coating
spellingShingle A. V. Kupryashov
Study of dynamics and rigidity of multifunctional coating of protective element of aircraft
Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
finite element method
stiffness
numerical simulation
vibration frequency
modal analysis
protective coating
title Study of dynamics and rigidity of multifunctional coating of protective element of aircraft
title_full Study of dynamics and rigidity of multifunctional coating of protective element of aircraft
title_fullStr Study of dynamics and rigidity of multifunctional coating of protective element of aircraft
title_full_unstemmed Study of dynamics and rigidity of multifunctional coating of protective element of aircraft
title_short Study of dynamics and rigidity of multifunctional coating of protective element of aircraft
title_sort study of dynamics and rigidity of multifunctional coating of protective element of aircraft
topic finite element method
stiffness
numerical simulation
vibration frequency
modal analysis
protective coating
url 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
work_keys_str_mv AT avkupryashov studyofdynamicsandrigidityofmultifunctionalcoatingofprotectiveelementofaircraft