On the dynamics of the turbulent flow past a three-element wing
A comprehensive analysis of the unsteady flow dynamics past the 30P30N three-element high lift wing is performed by means of large eddy simulations at different angles of attack (AoA=5°, 9°, and 23°) and at a Reynolds number of Rec=750.000 (based on the nested chord). Results are compared with exper...
| Autores: | , , |
|---|---|
| Tipo de recurso: | artículo |
| Fecha de publicación: | 2024 |
| País: | España |
| Institución: | Universitat Politècnica de Catalunya (UPC) |
| Repositorio: | UPCommons. Portal del coneixement obert de la UPC |
| Idioma: | inglés |
| OAI Identifier: | oai:upcommons.upc.edu:2117/402088 |
| Acceso en línea: | https://hdl.handle.net/2117/402088 https://dx.doi.org/https://doi.org/10.1063/5.0182215 |
| Access Level: | acceso abierto |
| Palabra clave: | Computational fluid dynamics High performance computing Turbulence Aerodynamics Airplanes--Wings High-lift device Flow instabilities Navier Stokes equations Flow dynamics Fluid drag Turbulence simulations Turbulent flows Dinàmica de fluids computacional Càlcul intensiu (Informàtica) Turbulència Aerodinàmica Avions--Ales Àrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluids Àrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica |
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| dc.title.none.fl_str_mv |
On the dynamics of the turbulent flow past a three-element wing |
| title |
On the dynamics of the turbulent flow past a three-element wing |
| spellingShingle |
On the dynamics of the turbulent flow past a three-element wing Montalà Sales, Ricard|||0009-0000-7911-7102 Computational fluid dynamics High performance computing Turbulence Aerodynamics Airplanes--Wings High-lift device High performance computing Computational fluid dynamics Aerodynamics Flow instabilities Navier Stokes equations Flow dynamics Fluid drag Turbulence simulations Turbulent flows Dinàmica de fluids computacional Càlcul intensiu (Informàtica) Turbulència Aerodinàmica Avions--Ales Àrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluids Àrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica |
| title_short |
On the dynamics of the turbulent flow past a three-element wing |
| title_full |
On the dynamics of the turbulent flow past a three-element wing |
| title_fullStr |
On the dynamics of the turbulent flow past a three-element wing |
| title_full_unstemmed |
On the dynamics of the turbulent flow past a three-element wing |
| title_sort |
On the dynamics of the turbulent flow past a three-element wing |
| dc.creator.none.fl_str_mv |
Montalà Sales, Ricard|||0009-0000-7911-7102 Lehmkuhl Barba, Oriol|||0000-0002-2670-1871 Rodríguez Pérez, Ivette María|||0000-0002-3749-277X |
| author |
Montalà Sales, Ricard|||0009-0000-7911-7102 |
| author_facet |
Montalà Sales, Ricard|||0009-0000-7911-7102 Lehmkuhl Barba, Oriol|||0000-0002-2670-1871 Rodríguez Pérez, Ivette María|||0000-0002-3749-277X |
| author_role |
author |
| author2 |
Lehmkuhl Barba, Oriol|||0000-0002-2670-1871 Rodríguez Pérez, Ivette María|||0000-0002-3749-277X |
| author2_role |
author author |
| dc.subject.none.fl_str_mv |
Computational fluid dynamics High performance computing Turbulence Aerodynamics Airplanes--Wings High-lift device High performance computing Computational fluid dynamics Aerodynamics Flow instabilities Navier Stokes equations Flow dynamics Fluid drag Turbulence simulations Turbulent flows Dinàmica de fluids computacional Càlcul intensiu (Informàtica) Turbulència Aerodinàmica Avions--Ales Àrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluids Àrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica |
| topic |
Computational fluid dynamics High performance computing Turbulence Aerodynamics Airplanes--Wings High-lift device High performance computing Computational fluid dynamics Aerodynamics Flow instabilities Navier Stokes equations Flow dynamics Fluid drag Turbulence simulations Turbulent flows Dinàmica de fluids computacional Càlcul intensiu (Informàtica) Turbulència Aerodinàmica Avions--Ales Àrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluids Àrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica |
| description |
A comprehensive analysis of the unsteady flow dynamics past the 30P30N three-element high lift wing is performed by means of large eddy simulations at different angles of attack (AoA=5°, 9°, and 23°) and at a Reynolds number of Rec=750.000 (based on the nested chord). Results are compared with experimental and numerical investigations, showing a quantitatively good agreement and, thus, proving the reliability and accuracy of the present simulations. Within the slat and main coves, large recirculation bubbles are bounded by shear layers, where the onset of turbulence is triggered by Kelvin–Helmholtz instabilities. In the energy spectrum of the velocity fluctuations, the footprint of these instabilities is detected as a broadband peak; its frequency being moved toward lower values as the angle of attack increases. Kelvin–Helmholtz vortices roll-up and break down into small scales that eventually impinge into the slat and main coves lower surfaces. The slat impingement shows to be more prominent, and hence, larger velocity and pressure fluctuations are observed. The impingement strength diminishes with the angle of attack in both coves, while higher fluctuations are originated on the slat and main respective suction sides, leading to larger boundary layers. This is associated with the displacement of the stagnation point with the angle of attack. Another salient feature observed is the laminar-to-turbulent flow transition in the main and flap leading edges although the average location of this transition seems to not be affected by the angle of attack. Tollmien–Schlichting instabilities precede this transition, with the disturbances amplified by the inviscid mode at low angles of attack, while at AoA=23°, the local Reynolds number on the main suction side is incremented and the viscous mode becomes important. The analysis shows that the turbulent wake formed at the trailing edge of all elements dominates the dynamics downstream. This is especially true at the higher angle of attack, where a large region of velocity deficit above the flap is observed, thus indicating the onset of stall conditions. |
| publishDate |
2024 |
| dc.date.none.fl_str_mv |
2024 2024-02-12 2024 2024-02-16 |
| dc.type.none.fl_str_mv |
journal article http://purl.org/coar/resource_type/c_6501 VoR http://purl.org/coar/version/c_970fb48d4fbd8a85 |
| dc.type.openaire.fl_str_mv |
info:eu-repo/semantics/article |
| format |
article |
| dc.identifier.none.fl_str_mv |
https://hdl.handle.net/2117/402088 https://dx.doi.org/https://doi.org/10.1063/5.0182215 |
| url |
https://hdl.handle.net/2117/402088 https://dx.doi.org/https://doi.org/10.1063/5.0182215 |
| dc.language.none.fl_str_mv |
Inglés eng |
| language_invalid_str_mv |
Inglés |
| language |
eng |
| dc.relation.none.fl_str_mv |
Agencia Estatal de Investigación http://doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020 PID2020-116937RB-C22 TOWARDS REAL-TIME ACTUATION STRATEGIES FOR FLOW CONTROL AND NOISE REDUCTION IN AIRCRAFTS. Agencia Estatal de Investigación http://doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020 PID2020-116937RB-C21 ALGORITMOS DE INTELIGENCIA ARTIFICIAL Y COMPUTACION DE ALTAS PRESTACIONES PARA MODELADO DE TURBULENCIA, CONTROL DE FLUJO Y AEROACUSTICA. |
| dc.rights.none.fl_str_mv |
open access http://purl.org/coar/access_right/c_abf2 Attribution 4.0 International http://creativecommons.org/licenses/by/4.0/ |
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info:eu-repo/semantics/openAccess |
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open access http://purl.org/coar/access_right/c_abf2 Attribution 4.0 International http://creativecommons.org/licenses/by/4.0/ |
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openAccess |
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application/pdf |
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reponame:UPCommons. Portal del coneixement obert de la UPC instname:Universitat Politècnica de Catalunya (UPC) |
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UPCommons. Portal del coneixement obert de la UPC |
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On the dynamics of the turbulent flow past a three-element wingMontalà Sales, Ricard|||0009-0000-7911-7102Lehmkuhl Barba, Oriol|||0000-0002-2670-1871Rodríguez Pérez, Ivette María|||0000-0002-3749-277XComputational fluid dynamicsHigh performance computingTurbulenceAerodynamicsAirplanes--WingsHigh-lift deviceHigh performance computingComputational fluid dynamicsAerodynamicsFlow instabilitiesNavier Stokes equationsFlow dynamicsFluid dragTurbulence simulationsTurbulent flowsDinàmica de fluids computacionalCàlcul intensiu (Informàtica)TurbulènciaAerodinàmicaAvions--AlesÀrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluidsÀrees temàtiques de la UPC::Aeronàutica i espai::AerodinàmicaA comprehensive analysis of the unsteady flow dynamics past the 30P30N three-element high lift wing is performed by means of large eddy simulations at different angles of attack (AoA=5°, 9°, and 23°) and at a Reynolds number of Rec=750.000 (based on the nested chord). Results are compared with experimental and numerical investigations, showing a quantitatively good agreement and, thus, proving the reliability and accuracy of the present simulations. Within the slat and main coves, large recirculation bubbles are bounded by shear layers, where the onset of turbulence is triggered by Kelvin–Helmholtz instabilities. In the energy spectrum of the velocity fluctuations, the footprint of these instabilities is detected as a broadband peak; its frequency being moved toward lower values as the angle of attack increases. Kelvin–Helmholtz vortices roll-up and break down into small scales that eventually impinge into the slat and main coves lower surfaces. The slat impingement shows to be more prominent, and hence, larger velocity and pressure fluctuations are observed. The impingement strength diminishes with the angle of attack in both coves, while higher fluctuations are originated on the slat and main respective suction sides, leading to larger boundary layers. This is associated with the displacement of the stagnation point with the angle of attack. Another salient feature observed is the laminar-to-turbulent flow transition in the main and flap leading edges although the average location of this transition seems to not be affected by the angle of attack. Tollmien–Schlichting instabilities precede this transition, with the disturbances amplified by the inviscid mode at low angles of attack, while at AoA=23°, the local Reynolds number on the main suction side is incremented and the viscous mode becomes important. The analysis shows that the turbulent wake formed at the trailing edge of all elements dominates the dynamics downstream. This is especially true at the higher angle of attack, where a large region of velocity deficit above the flap is observed, thus indicating the onset of stall conditions.This research has received financial support from the Ministerio de Ciencia e Innovación of Spain (Nos. PID2020-116937RB-C21 and PID2020-116937RB-C22). Furthermore, simulations were conducted with the assistance of the Red Española de Supercomputación (RES) and the EuroHPC JU, who granted us computational resources at the HPC facilities of MareNostrum IV, at Barcelona Supercomputing Center (IM-2022-3-0005), and Vega, at Institute of Information Science (REG- 2022R01-030), respectively. Finally, R. Montalà would like to express gratitude to the Departament de Recerca i Universitats de la Generalitat de Catalunya for awarding the FI-SDUR grant (No. 2022 FISDU 00066), which supports his doctoral studies.Peer Reviewed20242024-02-1220242024-02-16journal articlehttp://purl.org/coar/resource_type/c_6501VoRhttp://purl.org/coar/version/c_970fb48d4fbd8a85info:eu-repo/semantics/articleapplication/pdfhttps://hdl.handle.net/2117/402088https://dx.doi.org/https://doi.org/10.1063/5.0182215reponame:UPCommons. Portal del coneixement obert de la UPCinstname:Universitat Politècnica de Catalunya (UPC)InglésengAgencia Estatal de Investigación http://doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020 PID2020-116937RB-C22 TOWARDS REAL-TIME ACTUATION STRATEGIES FOR FLOW CONTROL AND NOISE REDUCTION IN AIRCRAFTS.Agencia Estatal de Investigación http://doi.org/10.13039/501100011033 Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020 PID2020-116937RB-C21 ALGORITMOS DE INTELIGENCIA ARTIFICIAL Y COMPUTACION DE ALTAS PRESTACIONES PARA MODELADO DE TURBULENCIA, CONTROL DE FLUJO Y AEROACUSTICA.open accesshttp://purl.org/coar/access_right/c_abf2Attribution 4.0 Internationalhttp://creativecommons.org/licenses/by/4.0/info:eu-repo/semantics/openAccessoai:upcommons.upc.edu:2117/4020882026-05-27T15:37:01Z |
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