No Cover Image

Journal article 547 views 790 downloads

Recent developments in the aeroelasticity of morphing aircraft

Rafic M. Ajaj, Muhammed S. Parancheerivilakkathil, Mohammadreza Amoozgar, Michael Friswell, Wesley J. Cantwell

Progress in Aerospace Sciences, Volume: 120, Start page: 100682

Swansea University Author: Michael Friswell

  • 56234.pdf

    PDF | Accepted Manuscript

    ©2020 All rights reserved. All article content, except where otherwise noted, is licensed under a Creative Commons Attribution Non-Commercial No Derivatives License (CC-BY-NC-ND)

    Download (5.27MB)

Check full text

DOI (Published version): 10.1016/j.paerosci.2020.100682

Abstract

This paper presents an extensive review of the developments in the aeroelasticity of morphing aircraft that occurred in the last decade (from 2009 to 2020). It focuses mainly on fixed-wing aircraft and highlights some representative examples from rotary-wing aircraft. Morphing wings are usually asso...

Full description

Published in: Progress in Aerospace Sciences
ISSN: 0376-0421
Published: Elsevier BV 2021
Online Access: Check full text

URI: https://cronfa.swan.ac.uk/Record/cronfa56234
Tags: Add Tag
No Tags, Be the first to tag this record!
first_indexed 2021-02-11T11:11:26Z
last_indexed 2021-03-03T04:21:21Z
id cronfa56234
recordtype SURis
fullrecord <?xml version="1.0"?><rfc1807><datestamp>2021-03-02T12:41:21.2005339</datestamp><bib-version>v2</bib-version><id>56234</id><entry>2021-02-11</entry><title>Recent developments in the aeroelasticity of morphing aircraft</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>2021-02-11</date><deptcode>FGSEN</deptcode><abstract>This paper presents an extensive review of the developments in the aeroelasticity of morphing aircraft that occurred in the last decade (from 2009 to 2020). It focuses mainly on fixed-wing aircraft and highlights some representative examples from rotary-wing aircraft. Morphing wings are usually associated with significant changes in the aerodynamic loads, structural/elastic properties, and inertial properties and hence the aeroelastic behavior. Changes in aeroelastic behavior can also affect the flight dynamics, stability, and control of air-vehicles. The main motivation for this paper is the fact that it is not fully possible to assess and quantify the benefits of morphing technologies without accounting for aeroelastic effects. The literature on the aeroelasticity of morphing aircraft can be split into two main themes: Aeroelastic Stability and Aeroelastic Control. The first theme (Aeroelastic Stability) includes studies conducted on morphing concepts to ensure that they satisfy certain aeroelastic requirements/constraints and that such requirements/constraints do not limit the potential benefits of morphing. The second theme (Aeroelastic Control) includes studies that utilized morphing technologies to improve aeroelastic characteristics and/or control flight loads. It is evident that in both themes, the aeroelasticity of morphing aircraft has been analyzed using analytical, numerical, and/or computational tools with a very limited number of wind-tunnel and/or flight tests. In this paper, research activities and studies are categorized according to the morphing degree of freedom they address. For each degree of freedom, research activities are arranged according to the theme they fit under. Aeroelastic frameworks developed for generic morphing applications are also reviewed. In addition, the aeroelastic models used are highlighted and discussed. Finally, trends and research gaps are identified and discussed and main conclusions are drawn.</abstract><type>Journal Article</type><journal>Progress in Aerospace Sciences</journal><volume>120</volume><journalNumber/><paginationStart>100682</paginationStart><paginationEnd/><publisher>Elsevier BV</publisher><placeOfPublication/><isbnPrint/><isbnElectronic/><issnPrint>0376-0421</issnPrint><issnElectronic/><keywords>Aeroelasticity, Morphing aircraft, UAVs, Flutter, Divergence, Loads alleviation</keywords><publishedDay>1</publishedDay><publishedMonth>1</publishedMonth><publishedYear>2021</publishedYear><publishedDate>2021-01-01</publishedDate><doi>10.1016/j.paerosci.2020.100682</doi><url/><notes/><college>COLLEGE NANME</college><department>Science and Engineering - Faculty</department><CollegeCode>COLLEGE CODE</CollegeCode><DepartmentCode>FGSEN</DepartmentCode><institution>Swansea University</institution><apcterm/><lastEdited>2021-03-02T12:41:21.2005339</lastEdited><Created>2021-02-11T11:09:49.1556667</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>Rafic M.</firstname><surname>Ajaj</surname><order>1</order></author><author><firstname>Muhammed S.</firstname><surname>Parancheerivilakkathil</surname><order>2</order></author><author><firstname>Mohammadreza</firstname><surname>Amoozgar</surname><order>3</order></author><author><firstname>Michael</firstname><surname>Friswell</surname><order>4</order></author><author><firstname>Wesley J.</firstname><surname>Cantwell</surname><order>5</order></author></authors><documents><document><filename>56234__19270__b0c3f63c8d914d4b82b62ccb6706bcbe.pdf</filename><originalFilename>56234.pdf</originalFilename><uploaded>2021-02-11T13:15:38.1097088</uploaded><type>Output</type><contentLength>5526776</contentLength><contentType>application/pdf</contentType><version>Accepted Manuscript</version><cronfaStatus>true</cronfaStatus><embargoDate>2022-02-09T00:00:00.0000000</embargoDate><documentNotes>&#xA9;2020 All rights reserved. All article content, except where otherwise noted, is licensed under a Creative Commons Attribution Non-Commercial No Derivatives License (CC-BY-NC-ND)</documentNotes><copyrightCorrect>true</copyrightCorrect><language>eng</language><licence>http://creativecommons.org/licenses/by-nc-nd/4.0/</licence></document></documents><OutputDurs/></rfc1807>
spelling 2021-03-02T12:41:21.2005339 v2 56234 2021-02-11 Recent developments in the aeroelasticity of morphing aircraft 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false 2021-02-11 FGSEN This paper presents an extensive review of the developments in the aeroelasticity of morphing aircraft that occurred in the last decade (from 2009 to 2020). It focuses mainly on fixed-wing aircraft and highlights some representative examples from rotary-wing aircraft. Morphing wings are usually associated with significant changes in the aerodynamic loads, structural/elastic properties, and inertial properties and hence the aeroelastic behavior. Changes in aeroelastic behavior can also affect the flight dynamics, stability, and control of air-vehicles. The main motivation for this paper is the fact that it is not fully possible to assess and quantify the benefits of morphing technologies without accounting for aeroelastic effects. The literature on the aeroelasticity of morphing aircraft can be split into two main themes: Aeroelastic Stability and Aeroelastic Control. The first theme (Aeroelastic Stability) includes studies conducted on morphing concepts to ensure that they satisfy certain aeroelastic requirements/constraints and that such requirements/constraints do not limit the potential benefits of morphing. The second theme (Aeroelastic Control) includes studies that utilized morphing technologies to improve aeroelastic characteristics and/or control flight loads. It is evident that in both themes, the aeroelasticity of morphing aircraft has been analyzed using analytical, numerical, and/or computational tools with a very limited number of wind-tunnel and/or flight tests. In this paper, research activities and studies are categorized according to the morphing degree of freedom they address. For each degree of freedom, research activities are arranged according to the theme they fit under. Aeroelastic frameworks developed for generic morphing applications are also reviewed. In addition, the aeroelastic models used are highlighted and discussed. Finally, trends and research gaps are identified and discussed and main conclusions are drawn. Journal Article Progress in Aerospace Sciences 120 100682 Elsevier BV 0376-0421 Aeroelasticity, Morphing aircraft, UAVs, Flutter, Divergence, Loads alleviation 1 1 2021 2021-01-01 10.1016/j.paerosci.2020.100682 COLLEGE NANME Science and Engineering - Faculty COLLEGE CODE FGSEN Swansea University 2021-03-02T12:41:21.2005339 2021-02-11T11:09:49.1556667 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised Rafic M. Ajaj 1 Muhammed S. Parancheerivilakkathil 2 Mohammadreza Amoozgar 3 Michael Friswell 4 Wesley J. Cantwell 5 56234__19270__b0c3f63c8d914d4b82b62ccb6706bcbe.pdf 56234.pdf 2021-02-11T13:15:38.1097088 Output 5526776 application/pdf Accepted Manuscript true 2022-02-09T00:00:00.0000000 ©2020 All rights reserved. All article content, except where otherwise noted, is licensed under a Creative Commons Attribution Non-Commercial No Derivatives License (CC-BY-NC-ND) true eng http://creativecommons.org/licenses/by-nc-nd/4.0/
title Recent developments in the aeroelasticity of morphing aircraft
spellingShingle Recent developments in the aeroelasticity of morphing aircraft
Michael Friswell
title_short Recent developments in the aeroelasticity of morphing aircraft
title_full Recent developments in the aeroelasticity of morphing aircraft
title_fullStr Recent developments in the aeroelasticity of morphing aircraft
title_full_unstemmed Recent developments in the aeroelasticity of morphing aircraft
title_sort Recent developments in the aeroelasticity of morphing aircraft
author_id_str_mv 5894777b8f9c6e64bde3568d68078d40
author_id_fullname_str_mv 5894777b8f9c6e64bde3568d68078d40_***_Michael Friswell
author Michael Friswell
author2 Rafic M. Ajaj
Muhammed S. Parancheerivilakkathil
Mohammadreza Amoozgar
Michael Friswell
Wesley J. Cantwell
format Journal article
container_title Progress in Aerospace Sciences
container_volume 120
container_start_page 100682
publishDate 2021
institution Swansea University
issn 0376-0421
doi_str_mv 10.1016/j.paerosci.2020.100682
publisher Elsevier BV
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 1
active_str 0
description This paper presents an extensive review of the developments in the aeroelasticity of morphing aircraft that occurred in the last decade (from 2009 to 2020). It focuses mainly on fixed-wing aircraft and highlights some representative examples from rotary-wing aircraft. Morphing wings are usually associated with significant changes in the aerodynamic loads, structural/elastic properties, and inertial properties and hence the aeroelastic behavior. Changes in aeroelastic behavior can also affect the flight dynamics, stability, and control of air-vehicles. The main motivation for this paper is the fact that it is not fully possible to assess and quantify the benefits of morphing technologies without accounting for aeroelastic effects. The literature on the aeroelasticity of morphing aircraft can be split into two main themes: Aeroelastic Stability and Aeroelastic Control. The first theme (Aeroelastic Stability) includes studies conducted on morphing concepts to ensure that they satisfy certain aeroelastic requirements/constraints and that such requirements/constraints do not limit the potential benefits of morphing. The second theme (Aeroelastic Control) includes studies that utilized morphing technologies to improve aeroelastic characteristics and/or control flight loads. It is evident that in both themes, the aeroelasticity of morphing aircraft has been analyzed using analytical, numerical, and/or computational tools with a very limited number of wind-tunnel and/or flight tests. In this paper, research activities and studies are categorized according to the morphing degree of freedom they address. For each degree of freedom, research activities are arranged according to the theme they fit under. Aeroelastic frameworks developed for generic morphing applications are also reviewed. In addition, the aeroelastic models used are highlighted and discussed. Finally, trends and research gaps are identified and discussed and main conclusions are drawn.
published_date 2021-01-01T04:11:02Z
_version_ 1763753761318109184
score 11.012678

Similar Items