Loading…
Application of Asymptotic and Numerical Methods to Determine Stability Boundaries of Distributed Systems in a Flow
The reasons and the set of parameters leading to aeroelastic flutter vibrations in distributed systems (DS) are investigated on the basis of asymptotic and numerical methods. The instability is caused by the combined influence of three factors: the drift of perturbations along the DS in the flow, be...
Saved in:
Published in: | Cybernetics and systems analysis 2022-03, Vol.58 (2), p.233-241 |
---|---|
Main Authors: | , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | cdi_FETCH-LOGICAL-c392t-6fa6e00b96f72822f260ff469f9e71b5443240215ece717c27a2b9f36555db73 |
---|---|
cites | cdi_FETCH-LOGICAL-c392t-6fa6e00b96f72822f260ff469f9e71b5443240215ece717c27a2b9f36555db73 |
container_end_page | 241 |
container_issue | 2 |
container_start_page | 233 |
container_title | Cybernetics and systems analysis |
container_volume | 58 |
creator | Kaliukh, I. Lebid, O. |
description | The reasons and the set of parameters leading to aeroelastic flutter vibrations in distributed systems (DS) are investigated on the basis of asymptotic and numerical methods. The instability is caused by the combined influence of three factors: the drift of perturbations along the DS in the flow, bending stiffness, and the influence of the inertial force, which is a distributed load moving along the DS. An increase in the tensile force and bending stiffness of the DS shifts the instability to a higher-frequency range of vibrations. An increase in the relative flux density and the relative length of the DS expands the region of instability. The presence of the angle of inclination of the DS to the flow adds peculiarities to the balance of forces acting on the DS and to the formation of the boundary ofstability and instability of regions. However, it is not possible to correctly assess its influence within the framework of the considered model and a more detailed further consideration is required. The configuration of the DS in the unstable region indicates the concentration of stresses near its upper end. The results obtained for small angles of inclination of the DS to the flow are consistent with the available results obtained by other authors. |
doi_str_mv | 10.1007/s10559-022-00455-0 |
format | article |
fullrecord | <record><control><sourceid>gale_proqu</sourceid><recordid>TN_cdi_proquest_journals_2689156306</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><galeid>A731239926</galeid><sourcerecordid>A731239926</sourcerecordid><originalsourceid>FETCH-LOGICAL-c392t-6fa6e00b96f72822f260ff469f9e71b5443240215ece717c27a2b9f36555db73</originalsourceid><addsrcrecordid>eNp9kcFu3CAQhq2qlZqmfYGekHrqwckABpbjNmnSSGkjZXNH2B62RLZxAavZty9bR6pyqTgMDN83IP1V9ZHCGQVQ54mCELoGxmqARogaXlUnVChebzhXr8seJNTAtXxbvUvpEQA4qM1JFbfzPPjOZh8mEhzZpsM455B9R-zUkx_LiLFcD-Q75p-hTyQHcokZ4-gnJLtsWz_4fCBfwjL1NnpMxymXPuXo2yVjT3aHlHFMxE_Ekqsh_H5fvXF2SPjhuZ5WD1dfHy6-1bd31zcX29u645rlWjorEaDV0im2YcwxCc41UjuNiraiaThrgFGBXTmrjinLWu24FEL0reKn1ad17BzDrwVTNo9hiVN50TC50VRIDrJQZyu1twMaP7mQo-3K6nH0XZjQ-dLfKk4Z15odhc8vhMJkfMp7u6Rkbnb3L1m2sl0MKUV0Zo5-tPFgKJhjbmbNzZTczN_cDBSJr1Iq8LTH-O_f_7H-AILfmgU</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2689156306</pqid></control><display><type>article</type><title>Application of Asymptotic and Numerical Methods to Determine Stability Boundaries of Distributed Systems in a Flow</title><source>Springer Link</source><creator>Kaliukh, I. ; Lebid, O.</creator><creatorcontrib>Kaliukh, I. ; Lebid, O.</creatorcontrib><description>The reasons and the set of parameters leading to aeroelastic flutter vibrations in distributed systems (DS) are investigated on the basis of asymptotic and numerical methods. The instability is caused by the combined influence of three factors: the drift of perturbations along the DS in the flow, bending stiffness, and the influence of the inertial force, which is a distributed load moving along the DS. An increase in the tensile force and bending stiffness of the DS shifts the instability to a higher-frequency range of vibrations. An increase in the relative flux density and the relative length of the DS expands the region of instability. The presence of the angle of inclination of the DS to the flow adds peculiarities to the balance of forces acting on the DS and to the formation of the boundary ofstability and instability of regions. However, it is not possible to correctly assess its influence within the framework of the considered model and a more detailed further consideration is required. The configuration of the DS in the unstable region indicates the concentration of stresses near its upper end. The results obtained for small angles of inclination of the DS to the flow are consistent with the available results obtained by other authors.</description><identifier>ISSN: 1060-0396</identifier><identifier>EISSN: 1573-8337</identifier><identifier>DOI: 10.1007/s10559-022-00455-0</identifier><language>eng</language><publisher>New York: Springer US</publisher><subject>Air-turbines ; Artificial Intelligence ; Asymptotic methods ; Asymptotic properties ; Bending ; Computer networks ; Control ; Flow stability ; Flutter ; Flux density ; Frequency ranges ; Inclination angle ; Mathematics ; Mathematics and Statistics ; Methods ; Numerical analysis ; Numerical methods ; Perturbation ; Processor Architectures ; Software Engineering/Programming and Operating Systems ; Stability analysis ; Stiffness ; Stress concentration ; Systems Theory</subject><ispartof>Cybernetics and systems analysis, 2022-03, Vol.58 (2), p.233-241</ispartof><rights>Springer Science+Business Media, LLC, part of Springer Nature 2022</rights><rights>COPYRIGHT 2022 Springer</rights><rights>Springer Science+Business Media, LLC, part of Springer Nature 2022.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c392t-6fa6e00b96f72822f260ff469f9e71b5443240215ece717c27a2b9f36555db73</citedby><cites>FETCH-LOGICAL-c392t-6fa6e00b96f72822f260ff469f9e71b5443240215ece717c27a2b9f36555db73</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Kaliukh, I.</creatorcontrib><creatorcontrib>Lebid, O.</creatorcontrib><title>Application of Asymptotic and Numerical Methods to Determine Stability Boundaries of Distributed Systems in a Flow</title><title>Cybernetics and systems analysis</title><addtitle>Cybern Syst Anal</addtitle><description>The reasons and the set of parameters leading to aeroelastic flutter vibrations in distributed systems (DS) are investigated on the basis of asymptotic and numerical methods. The instability is caused by the combined influence of three factors: the drift of perturbations along the DS in the flow, bending stiffness, and the influence of the inertial force, which is a distributed load moving along the DS. An increase in the tensile force and bending stiffness of the DS shifts the instability to a higher-frequency range of vibrations. An increase in the relative flux density and the relative length of the DS expands the region of instability. The presence of the angle of inclination of the DS to the flow adds peculiarities to the balance of forces acting on the DS and to the formation of the boundary ofstability and instability of regions. However, it is not possible to correctly assess its influence within the framework of the considered model and a more detailed further consideration is required. The configuration of the DS in the unstable region indicates the concentration of stresses near its upper end. The results obtained for small angles of inclination of the DS to the flow are consistent with the available results obtained by other authors.</description><subject>Air-turbines</subject><subject>Artificial Intelligence</subject><subject>Asymptotic methods</subject><subject>Asymptotic properties</subject><subject>Bending</subject><subject>Computer networks</subject><subject>Control</subject><subject>Flow stability</subject><subject>Flutter</subject><subject>Flux density</subject><subject>Frequency ranges</subject><subject>Inclination angle</subject><subject>Mathematics</subject><subject>Mathematics and Statistics</subject><subject>Methods</subject><subject>Numerical analysis</subject><subject>Numerical methods</subject><subject>Perturbation</subject><subject>Processor Architectures</subject><subject>Software Engineering/Programming and Operating Systems</subject><subject>Stability analysis</subject><subject>Stiffness</subject><subject>Stress concentration</subject><subject>Systems Theory</subject><issn>1060-0396</issn><issn>1573-8337</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp9kcFu3CAQhq2qlZqmfYGekHrqwckABpbjNmnSSGkjZXNH2B62RLZxAavZty9bR6pyqTgMDN83IP1V9ZHCGQVQ54mCELoGxmqARogaXlUnVChebzhXr8seJNTAtXxbvUvpEQA4qM1JFbfzPPjOZh8mEhzZpsM455B9R-zUkx_LiLFcD-Q75p-hTyQHcokZ4-gnJLtsWz_4fCBfwjL1NnpMxymXPuXo2yVjT3aHlHFMxE_Ekqsh_H5fvXF2SPjhuZ5WD1dfHy6-1bd31zcX29u645rlWjorEaDV0im2YcwxCc41UjuNiraiaThrgFGBXTmrjinLWu24FEL0reKn1ad17BzDrwVTNo9hiVN50TC50VRIDrJQZyu1twMaP7mQo-3K6nH0XZjQ-dLfKk4Z15odhc8vhMJkfMp7u6Rkbnb3L1m2sl0MKUV0Zo5-tPFgKJhjbmbNzZTczN_cDBSJr1Iq8LTH-O_f_7H-AILfmgU</recordid><startdate>20220301</startdate><enddate>20220301</enddate><creator>Kaliukh, I.</creator><creator>Lebid, O.</creator><general>Springer US</general><general>Springer</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>ISR</scope><scope>JQ2</scope></search><sort><creationdate>20220301</creationdate><title>Application of Asymptotic and Numerical Methods to Determine Stability Boundaries of Distributed Systems in a Flow</title><author>Kaliukh, I. ; Lebid, O.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c392t-6fa6e00b96f72822f260ff469f9e71b5443240215ece717c27a2b9f36555db73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Air-turbines</topic><topic>Artificial Intelligence</topic><topic>Asymptotic methods</topic><topic>Asymptotic properties</topic><topic>Bending</topic><topic>Computer networks</topic><topic>Control</topic><topic>Flow stability</topic><topic>Flutter</topic><topic>Flux density</topic><topic>Frequency ranges</topic><topic>Inclination angle</topic><topic>Mathematics</topic><topic>Mathematics and Statistics</topic><topic>Methods</topic><topic>Numerical analysis</topic><topic>Numerical methods</topic><topic>Perturbation</topic><topic>Processor Architectures</topic><topic>Software Engineering/Programming and Operating Systems</topic><topic>Stability analysis</topic><topic>Stiffness</topic><topic>Stress concentration</topic><topic>Systems Theory</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kaliukh, I.</creatorcontrib><creatorcontrib>Lebid, O.</creatorcontrib><collection>CrossRef</collection><collection>Gale In Context: Science</collection><collection>ProQuest Computer Science Collection</collection><jtitle>Cybernetics and systems analysis</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kaliukh, I.</au><au>Lebid, O.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Application of Asymptotic and Numerical Methods to Determine Stability Boundaries of Distributed Systems in a Flow</atitle><jtitle>Cybernetics and systems analysis</jtitle><stitle>Cybern Syst Anal</stitle><date>2022-03-01</date><risdate>2022</risdate><volume>58</volume><issue>2</issue><spage>233</spage><epage>241</epage><pages>233-241</pages><issn>1060-0396</issn><eissn>1573-8337</eissn><abstract>The reasons and the set of parameters leading to aeroelastic flutter vibrations in distributed systems (DS) are investigated on the basis of asymptotic and numerical methods. The instability is caused by the combined influence of three factors: the drift of perturbations along the DS in the flow, bending stiffness, and the influence of the inertial force, which is a distributed load moving along the DS. An increase in the tensile force and bending stiffness of the DS shifts the instability to a higher-frequency range of vibrations. An increase in the relative flux density and the relative length of the DS expands the region of instability. The presence of the angle of inclination of the DS to the flow adds peculiarities to the balance of forces acting on the DS and to the formation of the boundary ofstability and instability of regions. However, it is not possible to correctly assess its influence within the framework of the considered model and a more detailed further consideration is required. The configuration of the DS in the unstable region indicates the concentration of stresses near its upper end. The results obtained for small angles of inclination of the DS to the flow are consistent with the available results obtained by other authors.</abstract><cop>New York</cop><pub>Springer US</pub><doi>10.1007/s10559-022-00455-0</doi><tpages>9</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 1060-0396 |
ispartof | Cybernetics and systems analysis, 2022-03, Vol.58 (2), p.233-241 |
issn | 1060-0396 1573-8337 |
language | eng |
recordid | cdi_proquest_journals_2689156306 |
source | Springer Link |
subjects | Air-turbines Artificial Intelligence Asymptotic methods Asymptotic properties Bending Computer networks Control Flow stability Flutter Flux density Frequency ranges Inclination angle Mathematics Mathematics and Statistics Methods Numerical analysis Numerical methods Perturbation Processor Architectures Software Engineering/Programming and Operating Systems Stability analysis Stiffness Stress concentration Systems Theory |
title | Application of Asymptotic and Numerical Methods to Determine Stability Boundaries of Distributed Systems in a Flow |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-21T18%3A40%3A55IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-gale_proqu&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Application%20of%20Asymptotic%20and%20Numerical%20Methods%20to%20Determine%20Stability%20Boundaries%20of%20Distributed%20Systems%20in%20a%20Flow&rft.jtitle=Cybernetics%20and%20systems%20analysis&rft.au=Kaliukh,%20I.&rft.date=2022-03-01&rft.volume=58&rft.issue=2&rft.spage=233&rft.epage=241&rft.pages=233-241&rft.issn=1060-0396&rft.eissn=1573-8337&rft_id=info:doi/10.1007/s10559-022-00455-0&rft_dat=%3Cgale_proqu%3EA731239926%3C/gale_proqu%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c392t-6fa6e00b96f72822f260ff469f9e71b5443240215ece717c27a2b9f36555db73%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=2689156306&rft_id=info:pmid/&rft_galeid=A731239926&rfr_iscdi=true |