Analysis of UAS-S4 Éhecatl aerodynamic performance improvement using several configurations of a morphing wing technology
The paper presents the results of the aerodynamic optimisation of an Unmanned Aerial System's wing using a morphing approach. The shape deformation of the wing is achieved by placing actuator lines at several positions along its span. For each flight condition, the optimal displacements are fou...
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| Published in | Aeronautical journal Vol. 120; no. 1231; pp. 1337 - 1364 |
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| Main Authors | , , |
| Format | Journal Article |
| Language | English |
| Published |
Cambridge, UK
Cambridge University Press
01.09.2016
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| Subjects | |
| Online Access | Get full text |
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| Abstract | The paper presents the results of the aerodynamic optimisation of an Unmanned Aerial System's wing using a morphing approach. The shape deformation of the wing is achieved by placing actuator lines at several positions along its span. For each flight condition, the optimal displacements are found by using a combination of the new Artificial Bee Colony algorithm and a classical gradient-based search routine. The wing aerodynamic characteristics are calculated with an efficient nonlinear lifting line method coupled with a two-dimensional viscous flow solver. The optimisations are performed at angles of attack below the maximum lift angle, with the aim of improving the Hydra Technologies UAS-S4 wing lift-to-drag ratio. Several configurations of the morphing wing are proposed, each with a different number of actuation lines, and the improvements obtained by these configurations are analysed and compared. |
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| AbstractList | ABSTRACT
The paper presents the results of the aerodynamic optimisation of an Unmanned Aerial System's wing using a morphing approach. The shape deformation of the wing is achieved by placing actuator lines at several positions along its span. For each flight condition, the optimal displacements are found by using a combination of the new Artificial Bee Colony algorithm and a classical gradient-based search routine. The wing aerodynamic characteristics are calculated with an efficient nonlinear lifting line method coupled with a two-dimensional viscous flow solver. The optimisations are performed at angles of attack below the maximum lift angle, with the aim of improving the Hydra Technologies UAS-S4 wing lift-to-drag ratio. Several configurations of the morphing wing are proposed, each with a different number of actuation lines, and the improvements obtained by these configurations are analysed and compared. The paper presents the results of the aerodynamic optimisation of an Unmanned Aerial System's wing using a morphing approach. The shape deformation of the wing is achieved by placing actuator lines at several positions along its span. For each flight condition, the optimal displacements are found by using a combination of the new Artificial Bee Colony algorithm and a classical gradient-based search routine. The wing aerodynamic characteristics are calculated with an efficient nonlinear lifting line method coupled with a two-dimensional viscous flow solver. The optimisations are performed at angles of attack below the maximum lift angle, with the aim of improving the Hydra Technologies UAS-S4 wing lift-to-drag ratio. Several configurations of the morphing wing are proposed, each with a different number of actuation lines, and the improvements obtained by these configurations are analysed and compared. |
| Author | Botez, R.M. Koreanschi, A. Şugar Gabor, O. |
| Author_xml | – sequence: 1 givenname: O. surname: Şugar Gabor fullname: Şugar Gabor, O. email: oliviu.sugar-gabor.1@ens.etsmtl.ca organization: LARCASE (Laboratory of Applied Research in Active Controls), Avionics and Aeroservoelasticity, École de Technologie Supérieure, Department of Automated Production Engineering, Montréal, Québec, Canada – sequence: 2 givenname: A. surname: Koreanschi fullname: Koreanschi, A. email: andreea.koreanschi.1@ens.etsmtl.ca organization: LARCASE (Laboratory of Applied Research in Active Controls), Avionics and Aeroservoelasticity, École de Technologie Supérieure, Department of Automated Production Engineering, Montréal, Québec, Canada – sequence: 3 givenname: R.M. surname: Botez fullname: Botez, R.M. email: ruxandra@gpa.etsmtl.ca organization: Professor, Canada Research Chair in Aircraft Modeling and Simulation Technologies, LARCASE (Laboratory of Applied Research in Active Controls Avionics and Aeroservoelasticity), École de Technologie Supérieure, Department of Automated Production Engineering, Montréal, Québec, Canada |
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| Snippet | The paper presents the results of the aerodynamic optimisation of an Unmanned Aerial System's wing using a morphing approach. The shape deformation of the wing... ABSTRACT The paper presents the results of the aerodynamic optimisation of an Unmanned Aerial System's wing using a morphing approach. The shape deformation of... |
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| SubjectTerms | Actuation Aerodynamic characteristics Aerodynamics Aeronautics Aircraft Algorithms Angle of attack Automation Composite materials Configurations Deformation Design Laboratories Morphing Process engineering Search algorithms Studies Swarm intelligence Turbulence models Two dimensional flow Unmanned aerial vehicles Velocity Viscous flow Vortices |
| Title | Analysis of UAS-S4 Éhecatl aerodynamic performance improvement using several configurations of a morphing wing technology |
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