No Cover Image

Journal article 912 views

Aircraft Control via Variable Cant-Angle Winglets

P Bourdin, A Gatto, M. I Friswell, Michael Friswell

Journal of Aircraft, Volume: 45, Issue: 2, Pages: 414 - 423

Swansea University Author: Michael Friswell

Full text not available from this repository: check for access using links below.

Check full text

DOI (Published version): 10.2514/1.27720

Published in: Journal of Aircraft
ISSN: 0021-8669 1533-3868
Published: 2008
Online Access: Check full text

URI: https://cronfa.swan.ac.uk/Record/cronfa5504
Tags: Add Tag
No Tags, Be the first to tag this record!
first_indexed 2013-07-23T11:52:49Z
last_indexed 2018-02-09T04:31:51Z
id cronfa5504
recordtype SURis
fullrecord <?xml version="1.0"?><rfc1807><datestamp>2015-05-07T08:45:37.6306544</datestamp><bib-version>v2</bib-version><id>5504</id><entry>2013-09-03</entry><title>Aircraft Control via Variable Cant-Angle Winglets</title><swanseaauthors><author><sid>5894777b8f9c6e64bde3568d68078d40</sid><firstname>Michael</firstname><surname>Friswell</surname><name>Michael Friswell</name><active>true</active><ethesisStudent>false</ethesisStudent></author></swanseaauthors><date>2013-09-03</date><deptcode>FGSEN</deptcode><abstract></abstract><type>Journal Article</type><journal>Journal of Aircraft</journal><volume>45</volume><journalNumber>2</journalNumber><paginationStart>414</paginationStart><paginationEnd>423</paginationEnd><publisher/><issnPrint>0021-8669</issnPrint><issnElectronic>1533-3868</issnElectronic><keywords/><publishedDay>31</publishedDay><publishedMonth>12</publishedMonth><publishedYear>2008</publishedYear><publishedDate>2008-12-31</publishedDate><doi>10.2514/1.27720</doi><url/><notes>This paper formed part of the Marie-Curie Excellence grant on morphing aircraft (1.94M euros, 2005-2008) and was the first to consider using active winglets as control effectors. The investigation highlighted that novel aircraft configurations departed from the standard flight control approach of decoupling degrees of freedom and required a system view of such aircraft. This system level thinking was vital to the concept of the ERC Advanced Investigator grant on morphing aircraft (2.5M euros, 2010-2015).</notes><college>COLLEGE NANME</college><department>Science and Engineering - Faculty</department><CollegeCode>COLLEGE CODE</CollegeCode><DepartmentCode>FGSEN</DepartmentCode><institution>Swansea University</institution><apcterm/><lastEdited>2015-05-07T08:45:37.6306544</lastEdited><Created>2013-09-03T06:07:49.0000000</Created><path><level id="1">Faculty of Science and Engineering</level><level id="2">School of Engineering and Applied Sciences - Uncategorised</level></path><authors><author><firstname>P</firstname><surname>Bourdin</surname><order>1</order></author><author><firstname>A</firstname><surname>Gatto</surname><order>2</order></author><author><firstname>M. I</firstname><surname>Friswell</surname><order>3</order></author><author><firstname>Michael</firstname><surname>Friswell</surname><order>4</order></author></authors><documents/><OutputDurs/></rfc1807>
spelling 2015-05-07T08:45:37.6306544 v2 5504 2013-09-03 Aircraft Control via Variable Cant-Angle Winglets 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false 2013-09-03 FGSEN Journal Article Journal of Aircraft 45 2 414 423 0021-8669 1533-3868 31 12 2008 2008-12-31 10.2514/1.27720 This paper formed part of the Marie-Curie Excellence grant on morphing aircraft (1.94M euros, 2005-2008) and was the first to consider using active winglets as control effectors. The investigation highlighted that novel aircraft configurations departed from the standard flight control approach of decoupling degrees of freedom and required a system view of such aircraft. This system level thinking was vital to the concept of the ERC Advanced Investigator grant on morphing aircraft (2.5M euros, 2010-2015). COLLEGE NANME Science and Engineering - Faculty COLLEGE CODE FGSEN Swansea University 2015-05-07T08:45:37.6306544 2013-09-03T06:07:49.0000000 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised P Bourdin 1 A Gatto 2 M. I Friswell 3 Michael Friswell 4
title Aircraft Control via Variable Cant-Angle Winglets
spellingShingle Aircraft Control via Variable Cant-Angle Winglets
Michael Friswell
title_short Aircraft Control via Variable Cant-Angle Winglets
title_full Aircraft Control via Variable Cant-Angle Winglets
title_fullStr Aircraft Control via Variable Cant-Angle Winglets
title_full_unstemmed Aircraft Control via Variable Cant-Angle Winglets
title_sort Aircraft Control via Variable Cant-Angle Winglets
author_id_str_mv 5894777b8f9c6e64bde3568d68078d40
author_id_fullname_str_mv 5894777b8f9c6e64bde3568d68078d40_***_Michael Friswell
author Michael Friswell
author2 P Bourdin
A Gatto
M. I Friswell
Michael Friswell
format Journal article
container_title Journal of Aircraft
container_volume 45
container_issue 2
container_start_page 414
publishDate 2008
institution Swansea University
issn 0021-8669
1533-3868
doi_str_mv 10.2514/1.27720
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Engineering and Applied Sciences - Uncategorised{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Engineering and Applied Sciences - Uncategorised
document_store_str 0
active_str 0
published_date 2008-12-31T03:06:36Z
_version_ 1763749707078696960
score 11.012678

Similar Items