Experimental Investigation into Articulated Winglet Effects on Flying Wing Surface Pressure Aerodynamics

Gatto et al investigate the influence of articulated winglets on the resulting surface pressures on a flying wing test model for possible applications to gust load alleviation. The experimental model tested, analyzed, and evaluated used two actively controlled wingtips that were free to rotate about...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of aircraft 2010-09, Vol.47 (5), p.1811-1815
Hauptverfasser: Gatto, A, Bourdin, P, Friswell, M. I
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 1815
container_issue 5
container_start_page 1811
container_title Journal of aircraft
container_volume 47
creator Gatto, A
Bourdin, P
Friswell, M. I
description Gatto et al investigate the influence of articulated winglets on the resulting surface pressures on a flying wing test model for possible applications to gust load alleviation. The experimental model tested, analyzed, and evaluated used two actively controlled wingtips that were free to rotate about the wingtip chord axis line.
doi_str_mv 10.2514/1.C000251
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_crossref_primary_10_2514_1_C000251</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2170031181</sourcerecordid><originalsourceid>FETCH-LOGICAL-a317t-836b0ee4893eaff658b44823004746b3a3e8520e7e0fff0b627737f06ed844b83</originalsourceid><addsrcrecordid>eNplkEFLAzEQhYMoWKsH_0EQFDysJptskh5LabUgKKh4XGa3k5qy7tYkK_bfG23Rg6cZZr55j3mEnHJ2lRdcXvOrCWMstXtkwAshMmGU2SeDNOOZUWp0SI5CWCXGMK0H5HX6uUbv3rCN0NB5-4EhuiVE17XUtbGjYx9d3TcQcUFfXLtsMNKptVjHQBMzazZp-LOhj723UCN98BhC75GO0XeLTQtvrg7H5MBCE_BkV4fkeTZ9mtxmd_c388n4LgPBdcyMUBVDlGYkEKxVhamkNLlgTGqpKgECTZEz1MistaxSudZCW6ZwYaSsjBiSs63u2nfvffqmXHW9b5NlqYtRobjQKkGXW6j2XQgebblOGYDflJyV3zmWvNzlmNjznSCEGhrroa1d-D3IhUhQrhN3seXAAfyZ_hf8ApvDfbY</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>759561376</pqid></control><display><type>article</type><title>Experimental Investigation into Articulated Winglet Effects on Flying Wing Surface Pressure Aerodynamics</title><source>Alma/SFX Local Collection</source><creator>Gatto, A ; Bourdin, P ; Friswell, M. I</creator><creatorcontrib>Gatto, A ; Bourdin, P ; Friswell, M. I</creatorcontrib><description>Gatto et al investigate the influence of articulated winglets on the resulting surface pressures on a flying wing test model for possible applications to gust load alleviation. The experimental model tested, analyzed, and evaluated used two actively controlled wingtips that were free to rotate about the wingtip chord axis line.</description><identifier>ISSN: 0021-8669</identifier><identifier>EISSN: 1533-3868</identifier><identifier>DOI: 10.2514/1.C000251</identifier><identifier>CODEN: JAIRAM</identifier><language>eng</language><publisher>Reston, VA: American Institute of Aeronautics and Astronautics</publisher><subject>Aerodynamics ; Aerospace engineering ; Air transportation and traffic ; Aircraft ; Applied sciences ; Exact sciences and technology ; Experiments ; Ground, air and sea transportation, marine construction ; Wind tunnels</subject><ispartof>Journal of aircraft, 2010-09, Vol.47 (5), p.1811-1815</ispartof><rights>2015 INIST-CNRS</rights><rights>Copyright American Institute of Aeronautics and Astronautics Sep/Oct 2010</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a317t-836b0ee4893eaff658b44823004746b3a3e8520e7e0fff0b627737f06ed844b83</citedby><cites>FETCH-LOGICAL-a317t-836b0ee4893eaff658b44823004746b3a3e8520e7e0fff0b627737f06ed844b83</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&amp;idt=23351327$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Gatto, A</creatorcontrib><creatorcontrib>Bourdin, P</creatorcontrib><creatorcontrib>Friswell, M. I</creatorcontrib><title>Experimental Investigation into Articulated Winglet Effects on Flying Wing Surface Pressure Aerodynamics</title><title>Journal of aircraft</title><description>Gatto et al investigate the influence of articulated winglets on the resulting surface pressures on a flying wing test model for possible applications to gust load alleviation. The experimental model tested, analyzed, and evaluated used two actively controlled wingtips that were free to rotate about the wingtip chord axis line.</description><subject>Aerodynamics</subject><subject>Aerospace engineering</subject><subject>Air transportation and traffic</subject><subject>Aircraft</subject><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Experiments</subject><subject>Ground, air and sea transportation, marine construction</subject><subject>Wind tunnels</subject><issn>0021-8669</issn><issn>1533-3868</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2010</creationdate><recordtype>article</recordtype><recordid>eNplkEFLAzEQhYMoWKsH_0EQFDysJptskh5LabUgKKh4XGa3k5qy7tYkK_bfG23Rg6cZZr55j3mEnHJ2lRdcXvOrCWMstXtkwAshMmGU2SeDNOOZUWp0SI5CWCXGMK0H5HX6uUbv3rCN0NB5-4EhuiVE17XUtbGjYx9d3TcQcUFfXLtsMNKptVjHQBMzazZp-LOhj723UCN98BhC75GO0XeLTQtvrg7H5MBCE_BkV4fkeTZ9mtxmd_c388n4LgPBdcyMUBVDlGYkEKxVhamkNLlgTGqpKgECTZEz1MistaxSudZCW6ZwYaSsjBiSs63u2nfvffqmXHW9b5NlqYtRobjQKkGXW6j2XQgebblOGYDflJyV3zmWvNzlmNjznSCEGhrroa1d-D3IhUhQrhN3seXAAfyZ_hf8ApvDfbY</recordid><startdate>20100901</startdate><enddate>20100901</enddate><creator>Gatto, A</creator><creator>Bourdin, P</creator><creator>Friswell, M. I</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>U9A</scope></search><sort><creationdate>20100901</creationdate><title>Experimental Investigation into Articulated Winglet Effects on Flying Wing Surface Pressure Aerodynamics</title><author>Gatto, A ; Bourdin, P ; Friswell, M. I</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a317t-836b0ee4893eaff658b44823004746b3a3e8520e7e0fff0b627737f06ed844b83</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2010</creationdate><topic>Aerodynamics</topic><topic>Aerospace engineering</topic><topic>Air transportation and traffic</topic><topic>Aircraft</topic><topic>Applied sciences</topic><topic>Exact sciences and technology</topic><topic>Experiments</topic><topic>Ground, air and sea transportation, marine construction</topic><topic>Wind tunnels</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Gatto, A</creatorcontrib><creatorcontrib>Bourdin, P</creatorcontrib><creatorcontrib>Friswell, M. I</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>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of aircraft</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Gatto, A</au><au>Bourdin, P</au><au>Friswell, M. I</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental Investigation into Articulated Winglet Effects on Flying Wing Surface Pressure Aerodynamics</atitle><jtitle>Journal of aircraft</jtitle><date>2010-09-01</date><risdate>2010</risdate><volume>47</volume><issue>5</issue><spage>1811</spage><epage>1815</epage><pages>1811-1815</pages><issn>0021-8669</issn><eissn>1533-3868</eissn><coden>JAIRAM</coden><abstract>Gatto et al investigate the influence of articulated winglets on the resulting surface pressures on a flying wing test model for possible applications to gust load alleviation. The experimental model tested, analyzed, and evaluated used two actively controlled wingtips that were free to rotate about the wingtip chord axis line.</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.C000251</doi><tpages>5</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0021-8669
ispartof Journal of aircraft, 2010-09, Vol.47 (5), p.1811-1815
issn 0021-8669
1533-3868
language eng
recordid cdi_crossref_primary_10_2514_1_C000251
source Alma/SFX Local Collection
subjects Aerodynamics
Aerospace engineering
Air transportation and traffic
Aircraft
Applied sciences
Exact sciences and technology
Experiments
Ground, air and sea transportation, marine construction
Wind tunnels
title Experimental Investigation into Articulated Winglet Effects on Flying Wing Surface Pressure Aerodynamics
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-03T21%3A53%3A26IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Experimental%20Investigation%20into%20Articulated%20Winglet%20Effects%20on%20Flying%20Wing%20Surface%20Pressure%20Aerodynamics&rft.jtitle=Journal%20of%20aircraft&rft.au=Gatto,%20A&rft.date=2010-09-01&rft.volume=47&rft.issue=5&rft.spage=1811&rft.epage=1815&rft.pages=1811-1815&rft.issn=0021-8669&rft.eissn=1533-3868&rft.coden=JAIRAM&rft_id=info:doi/10.2514/1.C000251&rft_dat=%3Cproquest_cross%3E2170031181%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=759561376&rft_id=info:pmid/&rfr_iscdi=true