By-pass transition to airfoil flutter by transient growth due to gust impulse

We present an experimental study which shows that the mechanism known as transient growth of energy, can cause flutter instability of a nonlinearly flexible airfoil at a wind velocity below the linear critical flutter velocity. A flap mounted upstream a flexible airfoil in a wind tunnel generates a...

Full description

Saved in:
Bibliographic Details
Published in:Journal of fluids and structures 2009-11, Vol.25 (8), p.1272-1281
Main Authors: Schwartz, M., Manzoor, S., Hémon, P., de Langre, E.
Format: Article
Language:English
Subjects:
Aeroelasticity
By-pass transition
Engineering Sciences
Exact sciences and technology
Fluid mechanics
Fluids mechanics
Flutter
Fracture mechanics (crack, fatigue, damage...)
Fundamental areas of phenomenology (including applications)
Mechanics
Physics
Solid mechanics
Structural and continuum mechanics
Transient growth
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
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-c422t-455ec0057525e4c67f9f6297fba80e470bc1563c59085fe9d3c77c3c1a0ccfe13
cites cdi_FETCH-LOGICAL-c422t-455ec0057525e4c67f9f6297fba80e470bc1563c59085fe9d3c77c3c1a0ccfe13
container_end_page 1281
container_issue 8
container_start_page 1272
container_title Journal of fluids and structures
container_volume 25
creator Schwartz, M.
Manzoor, S.
Hémon, P.
de Langre, E.
description We present an experimental study which shows that the mechanism known as transient growth of energy, can cause flutter instability of a nonlinearly flexible airfoil at a wind velocity below the linear critical flutter velocity. A flap mounted upstream a flexible airfoil in a wind tunnel generates a single gust which triggers the plunge and pitch oscillations. This gust is characterized using two-component hot-wire anemometry. For the first time experimental evidence is provided to confirm the theoretical scenario of a by-pass transition to flutter by transient growth. From an engineering point of view, transient growth might explain also the premature structural fatigue encountered in structures subject to wind.
doi_str_mv 10.1016/j.jfluidstructs.2009.08.001
format article
fullrecord <record><control><sourceid>proquest_hal_p</sourceid><recordid>TN_cdi_hal_primary_oai_HAL_hal_01021128v1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S088997460900111X</els_id><sourcerecordid>35094958</sourcerecordid><originalsourceid>FETCH-LOGICAL-c422t-455ec0057525e4c67f9f6297fba80e470bc1563c59085fe9d3c77c3c1a0ccfe13</originalsourceid><addsrcrecordid>eNqNkE2LFDEQhsOisOPqf2gQBQ_dVtKd7gRP67IfwogXPYdMdWU3Q89kTNIr8-9NM8OCN-vyQvHUW_Aw9p5Dw4H3n7fN1k2zH1OOM-bUCADdgGoA-AVbcdCyVr0Qr9gKlNK1Hrr-kr1JaQsF7Fq-Yt-_HuuDTanK0e6Tzz7sqxwq66MLfqpKe84Uq83xDNA-V48x_MlP1TjTgj7OKVd-d5inRG_Za2dLvjvnFft1d_vz5qFe_7j_dnO9rrETItedlIQAcpBCUof94LTrhR7cxiqgboANctm3KDUo6UiPLQ4DtsgtIDri7RX7dOp9spM5RL-z8WiC9ebhem2WHXAQnAv1vLAfT-whht8zpWx2PiFNk91TmJNpZVGhpSrglxOIMaQUyb00czCLbrM1_-g2i24DyhTd5frD-Y1NaCdXbKFPLxWiTCd4W7jbE0fFz7OnaBIWq0ijj4TZjMH_17-_3oOeQg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>35094958</pqid></control><display><type>article</type><title>By-pass transition to airfoil flutter by transient growth due to gust impulse</title><source>ScienceDirect Freedom Collection</source><creator>Schwartz, M. ; Manzoor, S. ; Hémon, P. ; de Langre, E.</creator><creatorcontrib>Schwartz, M. ; Manzoor, S. ; Hémon, P. ; de Langre, E.</creatorcontrib><description>We present an experimental study which shows that the mechanism known as transient growth of energy, can cause flutter instability of a nonlinearly flexible airfoil at a wind velocity below the linear critical flutter velocity. A flap mounted upstream a flexible airfoil in a wind tunnel generates a single gust which triggers the plunge and pitch oscillations. This gust is characterized using two-component hot-wire anemometry. For the first time experimental evidence is provided to confirm the theoretical scenario of a by-pass transition to flutter by transient growth. From an engineering point of view, transient growth might explain also the premature structural fatigue encountered in structures subject to wind.</description><identifier>ISSN: 0889-9746</identifier><identifier>EISSN: 1095-8622</identifier><identifier>DOI: 10.1016/j.jfluidstructs.2009.08.001</identifier><identifier>CODEN: JFSTEF</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>Aeroelasticity ; By-pass transition ; Engineering Sciences ; Exact sciences and technology ; Fluid mechanics ; Fluids mechanics ; Flutter ; Fracture mechanics (crack, fatigue, damage...) ; Fundamental areas of phenomenology (including applications) ; Mechanics ; Physics ; Solid mechanics ; Structural and continuum mechanics ; Transient growth ; Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</subject><ispartof>Journal of fluids and structures, 2009-11, Vol.25 (8), p.1272-1281</ispartof><rights>2009 Elsevier Ltd</rights><rights>2015 INIST-CNRS</rights><rights>Distributed under a Creative Commons Attribution 4.0 International License</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c422t-455ec0057525e4c67f9f6297fba80e470bc1563c59085fe9d3c77c3c1a0ccfe13</citedby><cites>FETCH-LOGICAL-c422t-455ec0057525e4c67f9f6297fba80e470bc1563c59085fe9d3c77c3c1a0ccfe13</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,314,780,784,885,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&amp;idt=22224213$$DView record in Pascal Francis$$Hfree_for_read</backlink><backlink>$$Uhttps://polytechnique.hal.science/hal-01021128$$DView record in HAL$$Hfree_for_read</backlink></links><search><creatorcontrib>Schwartz, M.</creatorcontrib><creatorcontrib>Manzoor, S.</creatorcontrib><creatorcontrib>Hémon, P.</creatorcontrib><creatorcontrib>de Langre, E.</creatorcontrib><title>By-pass transition to airfoil flutter by transient growth due to gust impulse</title><title>Journal of fluids and structures</title><description>We present an experimental study which shows that the mechanism known as transient growth of energy, can cause flutter instability of a nonlinearly flexible airfoil at a wind velocity below the linear critical flutter velocity. A flap mounted upstream a flexible airfoil in a wind tunnel generates a single gust which triggers the plunge and pitch oscillations. This gust is characterized using two-component hot-wire anemometry. For the first time experimental evidence is provided to confirm the theoretical scenario of a by-pass transition to flutter by transient growth. From an engineering point of view, transient growth might explain also the premature structural fatigue encountered in structures subject to wind.</description><subject>Aeroelasticity</subject><subject>By-pass transition</subject><subject>Engineering Sciences</subject><subject>Exact sciences and technology</subject><subject>Fluid mechanics</subject><subject>Fluids mechanics</subject><subject>Flutter</subject><subject>Fracture mechanics (crack, fatigue, damage...)</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Mechanics</subject><subject>Physics</subject><subject>Solid mechanics</subject><subject>Structural and continuum mechanics</subject><subject>Transient growth</subject><subject>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</subject><issn>0889-9746</issn><issn>1095-8622</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2009</creationdate><recordtype>article</recordtype><recordid>eNqNkE2LFDEQhsOisOPqf2gQBQ_dVtKd7gRP67IfwogXPYdMdWU3Q89kTNIr8-9NM8OCN-vyQvHUW_Aw9p5Dw4H3n7fN1k2zH1OOM-bUCADdgGoA-AVbcdCyVr0Qr9gKlNK1Hrr-kr1JaQsF7Fq-Yt-_HuuDTanK0e6Tzz7sqxwq66MLfqpKe84Uq83xDNA-V48x_MlP1TjTgj7OKVd-d5inRG_Za2dLvjvnFft1d_vz5qFe_7j_dnO9rrETItedlIQAcpBCUof94LTrhR7cxiqgboANctm3KDUo6UiPLQ4DtsgtIDri7RX7dOp9spM5RL-z8WiC9ebhem2WHXAQnAv1vLAfT-whht8zpWx2PiFNk91TmJNpZVGhpSrglxOIMaQUyb00czCLbrM1_-g2i24DyhTd5frD-Y1NaCdXbKFPLxWiTCd4W7jbE0fFz7OnaBIWq0ijj4TZjMH_17-_3oOeQg</recordid><startdate>20091101</startdate><enddate>20091101</enddate><creator>Schwartz, M.</creator><creator>Manzoor, S.</creator><creator>Hémon, P.</creator><creator>de Langre, E.</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>KR7</scope><scope>L7M</scope><scope>1XC</scope></search><sort><creationdate>20091101</creationdate><title>By-pass transition to airfoil flutter by transient growth due to gust impulse</title><author>Schwartz, M. ; Manzoor, S. ; Hémon, P. ; de Langre, E.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c422t-455ec0057525e4c67f9f6297fba80e470bc1563c59085fe9d3c77c3c1a0ccfe13</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2009</creationdate><topic>Aeroelasticity</topic><topic>By-pass transition</topic><topic>Engineering Sciences</topic><topic>Exact sciences and technology</topic><topic>Fluid mechanics</topic><topic>Fluids mechanics</topic><topic>Flutter</topic><topic>Fracture mechanics (crack, fatigue, damage...)</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Mechanics</topic><topic>Physics</topic><topic>Solid mechanics</topic><topic>Structural and continuum mechanics</topic><topic>Transient growth</topic><topic>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Schwartz, M.</creatorcontrib><creatorcontrib>Manzoor, S.</creatorcontrib><creatorcontrib>Hémon, P.</creatorcontrib><creatorcontrib>de Langre, E.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Hyper Article en Ligne (HAL)</collection><jtitle>Journal of fluids and structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Schwartz, M.</au><au>Manzoor, S.</au><au>Hémon, P.</au><au>de Langre, E.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>By-pass transition to airfoil flutter by transient growth due to gust impulse</atitle><jtitle>Journal of fluids and structures</jtitle><date>2009-11-01</date><risdate>2009</risdate><volume>25</volume><issue>8</issue><spage>1272</spage><epage>1281</epage><pages>1272-1281</pages><issn>0889-9746</issn><eissn>1095-8622</eissn><coden>JFSTEF</coden><abstract>We present an experimental study which shows that the mechanism known as transient growth of energy, can cause flutter instability of a nonlinearly flexible airfoil at a wind velocity below the linear critical flutter velocity. A flap mounted upstream a flexible airfoil in a wind tunnel generates a single gust which triggers the plunge and pitch oscillations. This gust is characterized using two-component hot-wire anemometry. For the first time experimental evidence is provided to confirm the theoretical scenario of a by-pass transition to flutter by transient growth. From an engineering point of view, transient growth might explain also the premature structural fatigue encountered in structures subject to wind.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.jfluidstructs.2009.08.001</doi><tpages>10</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0889-9746
ispartof Journal of fluids and structures, 2009-11, Vol.25 (8), p.1272-1281
issn 0889-9746
1095-8622
language eng
recordid cdi_hal_primary_oai_HAL_hal_01021128v1
source ScienceDirect Freedom Collection
subjects Aeroelasticity
By-pass transition
Engineering Sciences
Exact sciences and technology
Fluid mechanics
Fluids mechanics
Flutter
Fracture mechanics (crack, fatigue, damage...)
Fundamental areas of phenomenology (including applications)
Mechanics
Physics
Solid mechanics
Structural and continuum mechanics
Transient growth
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
title By-pass transition to airfoil flutter by transient growth due to gust impulse
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-20T13%3A56%3A04IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_hal_p&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=By-pass%20transition%20to%20airfoil%20flutter%20by%20transient%20growth%20due%20to%20gust%20impulse&rft.jtitle=Journal%20of%20fluids%20and%20structures&rft.au=Schwartz,%20M.&rft.date=2009-11-01&rft.volume=25&rft.issue=8&rft.spage=1272&rft.epage=1281&rft.pages=1272-1281&rft.issn=0889-9746&rft.eissn=1095-8622&rft.coden=JFSTEF&rft_id=info:doi/10.1016/j.jfluidstructs.2009.08.001&rft_dat=%3Cproquest_hal_p%3E35094958%3C/proquest_hal_p%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c422t-455ec0057525e4c67f9f6297fba80e470bc1563c59085fe9d3c77c3c1a0ccfe13%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=35094958&rft_id=info:pmid/&rfr_iscdi=true