Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control

In this study, the morphing technology was applied on winglets for the CRJ-700 transport regional aircraft with the aim to improve its aerodynamic performance. The LARCASE Virtual Research Simulator VRESIM is equipped with highest Level D certified flight data for the CRJ-700. The flight and geometr...

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Autores principales:	Paul MEYRAN, Hugo PAIN, Ruxandra Mihaela BOTEZ, Jeremy LALIBERTÉ
Formato:	article
Lenguaje:	EN
Publicado:	National Institute for Aerospace Research “Elie Carafoli” - INCAS 2021
Materias:	design morphing winglet aerodynamics structure optimization control Motor vehicles. Aeronautics. Astronautics TL1-4050
Acceso en línea:	https://doaj.org/article/46e1a9233ea34dc395eaafa864c841be
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id	oai:doaj.org-article:46e1a9233ea34dc395eaafa864c841be
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spelling	oai:doaj.org-article:46e1a9233ea34dc395eaafa864c841be2021-12-05T21:26:53ZStructural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control10.13111/2066-8201.2021.13.4.112066-82012247-4528https://doaj.org/article/46e1a9233ea34dc395eaafa864c841be2021-12-01T00:00:00Zhttps://bulletin.incas.ro/files/meyran_pain_botez_laliberte_part_2_vol_13_iss_4.pdfhttps://doaj.org/toc/2066-8201https://doaj.org/toc/2247-4528In this study, the morphing technology was applied on winglets for the CRJ-700 transport regional aircraft with the aim to improve its aerodynamic performance. The LARCASE Virtual Research Simulator VRESIM is equipped with highest Level D certified flight data for the CRJ-700. The flight and geometrical data of the CRJ-700 were used to quantify the aerodynamic benefits of the CRJ-700 equipped with a morphing winglet versus its reference winglet. The structural design and the mechanism allowing its rotation were used to allow the orientation of the winglet with angles between 90° and -90°. The control of the orientation of the morphing winglet with its mechanism was finally carried out using the Matlab/ Simulink interface. Therefore, a new concept of morphing winglet was obtained in this research.Paul MEYRANHugo PAINRuxandra Mihaela BOTEZJeremy LALIBERTÉNational Institute for Aerospace Research “Elie Carafoli” - INCASarticledesignmorphing wingletaerodynamicsstructureoptimizationcontrolMotor vehicles. Aeronautics. AstronauticsTL1-4050ENINCAS Bulletin, Pp 129-137 (2021)
institution	DOAJ
collection	DOAJ
language	EN
topic	design morphing winglet aerodynamics structure optimization control Motor vehicles. Aeronautics. Astronautics TL1-4050
spellingShingle	design morphing winglet aerodynamics structure optimization control Motor vehicles. Aeronautics. Astronautics TL1-4050 Paul MEYRAN Hugo PAIN Ruxandra Mihaela BOTEZ Jeremy LALIBERTÉ Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control
description	In this study, the morphing technology was applied on winglets for the CRJ-700 transport regional aircraft with the aim to improve its aerodynamic performance. The LARCASE Virtual Research Simulator VRESIM is equipped with highest Level D certified flight data for the CRJ-700. The flight and geometrical data of the CRJ-700 were used to quantify the aerodynamic benefits of the CRJ-700 equipped with a morphing winglet versus its reference winglet. The structural design and the mechanism allowing its rotation were used to allow the orientation of the winglet with angles between 90° and -90°. The control of the orientation of the morphing winglet with its mechanism was finally carried out using the Matlab/ Simulink interface. Therefore, a new concept of morphing winglet was obtained in this research.
format	article
author	Paul MEYRAN Hugo PAIN Ruxandra Mihaela BOTEZ Jeremy LALIBERTÉ
author_facet	Paul MEYRAN Hugo PAIN Ruxandra Mihaela BOTEZ Jeremy LALIBERTÉ
author_sort	Paul MEYRAN
title	Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control
title_short	Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control
title_full	Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control
title_fullStr	Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control
title_full_unstemmed	Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control
title_sort	structural design and control of a morphing winglet to optimize the aerodynamic performance of the crj-700 aircraft. part 2 – control
publisher	National Institute for Aerospace Research “Elie Carafoli” - INCAS
publishDate	2021
url	https://doaj.org/article/46e1a9233ea34dc395eaafa864c841be
work_keys_str_mv	AT paulmeyran structuraldesignandcontrolofamorphingwinglettooptimizetheaerodynamicperformanceofthecrj700aircraftpart2control AT hugopain structuraldesignandcontrolofamorphingwinglettooptimizetheaerodynamicperformanceofthecrj700aircraftpart2control AT ruxandramihaelabotez structuraldesignandcontrolofamorphingwinglettooptimizetheaerodynamicperformanceofthecrj700aircraftpart2control AT jeremylaliberte structuraldesignandcontrolofamorphingwinglettooptimizetheaerodynamicperformanceofthecrj700aircraftpart2control
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Structural Design and Control of a Morphing Winglet to optimize the Aerodynamic Performance of the CRJ-700 Aircraft. Part 2 – Control

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