Conference Paper/Proceeding/Abstract 736 views
THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING
XI International Conference on Structural Dynamics, Volume: 1, Pages: 631 - 639
Swansea University Authors:
Davide Balatti, Hamed Haddad Khodaparast , Michael Friswell, Marinos Manolesos
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DOI (Published version): 10.47964/1120.9050.19773
Abstract
In recent years, the development of lighter and more efficient transport aircraft has led to an increased focus on gust load alleviation. A recent strategy is based on the use of folding wingtip devices that increase the aspect ratio and therefore improves the aircraft performance. Moreover, numeric...
Published in: | XI International Conference on Structural Dynamics |
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ISBN: | 9786188507203, 9786188507227 |
ISSN: | 2311-9020 |
Published: |
Athens
EASD
2020
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URI: | https://cronfa.swan.ac.uk/Record/cronfa57476 |
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2021-09-27T10:47:06.7887018 v2 57476 2021-07-29 THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING 4c58ba20bbabfef44b00b143e96b37e1 Davide Balatti Davide Balatti true false f207b17edda9c4c3ea074cbb7555efc1 0000-0002-3721-4980 Hamed Haddad Khodaparast Hamed Haddad Khodaparast true false 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false 44a3e0d351ccd7a8365d5fc7c50c8778 Marinos Manolesos Marinos Manolesos true false 2021-07-29 AERO In recent years, the development of lighter and more efficient transport aircraft has led to an increased focus on gust load alleviation. A recent strategy is based on the use of folding wingtip devices that increase the aspect ratio and therefore improves the aircraft performance. Moreover, numerical studies have suggested such a folding wingtip solution may incorporate spring devices in order to provide additional gust load alleviation ability in flight. It has been shown that wingtip mass, stiffness connection and hinge orientation are key parameters to avoid flutter and achieve load alleviation during gusts. In this paper, after defining a simplified aeroelastic model representative of an symmetric aircraft, considers the case of adding movable wingtips. The effects of hinge position, orientation and spring stiffness will be considered in order to evaluate the potential of this technique for gust load alleviation. Moreover, is studied the longitudinal flight dynamics of a rigid aircraft with elastic wing Conference Paper/Proceeding/Abstract XI International Conference on Structural Dynamics 1 631 639 EASD Athens 9786188507203, 9786188507227 2311-9020 Aeroelasticity, gust load alleviation, folding wingtip, passive control 1 9 2020 2020-09-01 10.47964/1120.9050.19773 Available as full-text from the EASD (European Association for Structural Dynamics- EURODYN 2020) website. COLLEGE NANME Aerospace Engineering COLLEGE CODE AERO Swansea University Engineering Physical Science Research Council (EPSRC) through a programme grant. EP/R006768/1 2021-09-27T10:47:06.7887018 2021-07-29T17:03:42.1655549 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised Davide Balatti 1 Hamed Haddad Khodaparast 0000-0002-3721-4980 2 Michael Friswell 3 Marinos Manolesos 4 Mohammadreza Amoozgar 5 |
title |
THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING |
spellingShingle |
THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING Davide Balatti Hamed Haddad Khodaparast Michael Friswell Marinos Manolesos |
title_short |
THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING |
title_full |
THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING |
title_fullStr |
THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING |
title_full_unstemmed |
THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING |
title_sort |
THE EFFECT OF FOLDING WINGTIPS ON THE FLIGHT DYNAMICS OF AN AIRCRAFT WITH ELASTIC WING |
author_id_str_mv |
4c58ba20bbabfef44b00b143e96b37e1 f207b17edda9c4c3ea074cbb7555efc1 5894777b8f9c6e64bde3568d68078d40 44a3e0d351ccd7a8365d5fc7c50c8778 |
author_id_fullname_str_mv |
4c58ba20bbabfef44b00b143e96b37e1_***_Davide Balatti f207b17edda9c4c3ea074cbb7555efc1_***_Hamed Haddad Khodaparast 5894777b8f9c6e64bde3568d68078d40_***_Michael Friswell 44a3e0d351ccd7a8365d5fc7c50c8778_***_Marinos Manolesos |
author |
Davide Balatti Hamed Haddad Khodaparast Michael Friswell Marinos Manolesos |
author2 |
Davide Balatti Hamed Haddad Khodaparast Michael Friswell Marinos Manolesos Mohammadreza Amoozgar |
format |
Conference Paper/Proceeding/Abstract |
container_title |
XI International Conference on Structural Dynamics |
container_volume |
1 |
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631 |
publishDate |
2020 |
institution |
Swansea University |
isbn |
9786188507203, 9786188507227 |
issn |
2311-9020 |
doi_str_mv |
10.47964/1120.9050.19773 |
publisher |
EASD |
college_str |
Faculty of Science and Engineering |
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facultyofscienceandengineering |
hierarchy_top_title |
Faculty of Science and Engineering |
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facultyofscienceandengineering |
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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 |
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description |
In recent years, the development of lighter and more efficient transport aircraft has led to an increased focus on gust load alleviation. A recent strategy is based on the use of folding wingtip devices that increase the aspect ratio and therefore improves the aircraft performance. Moreover, numerical studies have suggested such a folding wingtip solution may incorporate spring devices in order to provide additional gust load alleviation ability in flight. It has been shown that wingtip mass, stiffness connection and hinge orientation are key parameters to avoid flutter and achieve load alleviation during gusts. In this paper, after defining a simplified aeroelastic model representative of an symmetric aircraft, considers the case of adding movable wingtips. The effects of hinge position, orientation and spring stiffness will be considered in order to evaluate the potential of this technique for gust load alleviation. Moreover, is studied the longitudinal flight dynamics of a rigid aircraft with elastic wing |
published_date |
2020-09-01T04:13:15Z |
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1763753900280643584 |
score |
11.012678 |