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Enregistrement W4224948513 · doi:10.2514/1.j061405

Coupled High Pressure-Temperature Effects on Performance of Dielectric Barrier Discharge Actuators

2022· article· en· W4224948513 sur OpenAlexafffundabout
Hassen Dammak, Philippe Versailles, Huu Duc Vo

Notice bibliographique

RevueAIAA Journal · 2022
Typearticle
Langueen
DomaineEngineering
ThématiquePlasma and Flow Control in Aerodynamics
Établissements canadiensPolytechnique Montréal
Organismes subventionnairesNatural Sciences and Engineering Research Council of Canada
Mots-clésDielectric barrier dischargeAirfoilPlasma actuatorDielectricMaterials scienceEngineering physicsMechanical engineeringHumanitiesPhysicsEngineeringElectrical engineeringArtAerospace engineering

Résumé

récupéré en direct d'OpenAlex

No AccessTechnical NotesCoupled High Pressure-Temperature Effects on Performance of Dielectric Barrier Discharge ActuatorsHassen Dammak, Philippe Versailles and Huu Duc VoHassen DammakPolytechnique Montreal, Montreal, Quebec H3T 1 J4, Canada, Philippe VersaillesPolytechnique Montreal, Montreal, Quebec H3T 1 J4, Canada and Huu Duc VoPolytechnique Montreal, Montreal, Quebec H3T 1 J4, CanadaPublished Online:27 Apr 2022https://doi.org/10.2514/1.J061405SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Enloe C. L., McLaughlin T. E., Van Dyken R. D., Kachner K. D., Jumper E. J. and Corke T., "Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology," AIAA Journal, Vol. 42, No. 3, 2004, pp. 589–594. https://doi.org/10.2514/1.2305 LinkGoogle Scholar[2] Shyy W., Jayaraman B. and Andersson A., "Modeling of Glow Discharge-Induced Fluid Dynamics," Journal of Applied Physics, Vol. 92, No. 11, 2002, pp. 6434–6443. https://doi.org/10.1063/1.1515103 CrossrefGoogle Scholar[3] Post M., andCorke T. C., "Separation Control on High Angle of Attack Airfoil Using Plasma Actuators," AIAA Journal, Vol. 42, No. 11, 2004, pp. 2177–2184. https://doi.org/10.2514/1.2929 LinkGoogle Scholar[4] Boesch G., Vo H. D., Savard B., Wanko-Tchatchouang C. and Mureithi N. W., "Flight Control Using Wing Tip Plasma Actuation," Journal of Aircraft, Vol. 47, No. 6, 2010, pp. 1836–1846. https://doi.org/10.2514/1.44003 LinkGoogle Scholar[5] Huang J., Corke T. C. and Thomas F. O., "Plasma Actuators for Separation Control of Low-Pressure Turbine Blades," AIAA Journal, Vol. 44, No. 1, 2006, pp. 51–57. https://doi.org/10.2514/1.2903 LinkGoogle Scholar[6] Akçayoz E., Vo H. D. and Mahallati A., "Controlling Corner Stall Separation with Plasma Actuators in a Compressor Cascade," Journal of Turbomachinery, Vol. 138, No. 8, 2016, pp. 1–13. https://doi.org/10.1115/1.4032675 Google Scholar[7] Morris S., Corke T., VanNess D., Stephens J. and Douville T., "Tip Clearance Control Using Plasma Actuator," AIAA Paper 2005-0782, 2005. https://doi.org/10.2514/6.2005-782 Google Scholar[8] Lemire S. and Vo H. D., "Reduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction," Journal of Turbomachinery, Vol. 133, No. 1, 2011, pp. 1–11. https://doi.org/10.1115/1.4000540 Google Scholar[9] Jothiprasad G., Murray R. C., Essenhigh K., Bennett G. A., Saddoughi S., Wadia A. and Breeze-Stringfellow A., "Control of Tip-Clearance Flow in a Low Speed Axial Compressor Rotor with Plasma Actuation," Journal of Turbomachinery, Vol. 134, No. 2, 2012, pp. 1–9. https://doi.org/10.1115/1.4003083 Google Scholar[10] Ashrafi F., Michaud M. and Vo H. D., "Delay of Rotating Stall in Compressors With Plasma Actuators," Journal of Turbomachinery, Vol. 138, No. 9, 2016, pp. 1–12. https://doi.org/10.1115/1.4032840 Google Scholar[11] Wang L., Wong C. W., Lu Z., Wu Z. and Zhou Y., "Novel Sawtooth Dielectric Barrier Discharge Plasma Actuator for Flow Separation Control," AIAA Journal, Vol. 55, No. 4, 2017, pp. 1405–1416. https://doi.org/10.2514/1.J055507 LinkGoogle Scholar[12] Zoppini G., Belan M., Zanotti A., Di Vinci L. and Campanardi G., "Stall Control by Plasma Actuators: Characterization Along the Airfoil Span," Energies, Vol. 13, No. 6, 2020. https://doi.org/10.3390/en13061374 CrossrefGoogle Scholar[13] Xu S. Y., Cai J. S., Wang J. F. and Tang S. J., "Characterization of the Single Nanosecond Pulsed Surface Dielectric Barrier Plasma Actuator: Geometric and Electric Effects," Contributions to Plasma Physics, Vol. 60, No. 7, 2020, pp. 1–13. https://doi.org/10.1002/ctpp.201900081 Google Scholar[14] Schuele C.-Y. and Corke T., "Characteristics of Single Dielectric Barrier Discharge Plasma Actuators at Subatmospheric Pressures," 61st Annual Meeting of the APS Division of Fluid Dynamics, American Physical Soc., Nov. 2008. Google Scholar[15] Gregory J. W., Enloe C. L., Font G. I. and McLaughlin T. E., "Force Production Mechanisms of a Dielectric-Barrier Discharge Plasma Actuator," AIAA Paper 2007-0185, 2007. https://doi.org/10.2514/6.2007-185 LinkGoogle Scholar[16] Benard N., Balcon N. and Moreau E., "Electric Wind Produced by a Surface Dielectric Barrier Discharge Operating in Air at Different Pressures: Aeronautical Control Insights," Journal of Physics D: Applied Physics, Vol. 41, No. 4, 2008, pp. 1–5. https://doi.org/10.1088/0022-3727/41/4/042002 Google Scholar[17] Abe T., Takizawa Y., Sato S. and Kimura N., "A Parametric Experimental Study for Momentum Transfer by Plasma Actuator," AIAA Paper 2007-0187, 2007. https://doi.org/10.2514/6.2007-187 LinkGoogle Scholar[18] Segawa T., Furutani H. and Yoshida H., "Wall Normal Jet Under Elevated Temperatures Produced by Surface Plasma Actuator," AIAA Paper 2007-0784, 2007. https://doi.org/10.2514/6.2007-784 Google Scholar[19] Versailles P., Gingras-Gosselin V. and Vo H. D., "Impact of Pressure and Temperature on the Performance of Plasma Actuators," AIAA Journal, Vol. 48, No. 4, 2010, pp. 859–863. https://doi.org/10.2514/1.43852 LinkGoogle Scholar[20] Valerioti J. A. and Corke T. C., "Pressure Dependence of Dielectric Barrier Discharge Plasma Flow Actuators," AIAA Journal, Vol. 50, No. 7, 2012, pp. 1490–1502. https://doi.org/10.2514/1.J051194 LinkGoogle Scholar[21] Ashpis D. E. and Thurman D. R., "Dielectric Barrier Discharge (DBD) Plasma Actuators for Flow Control in Turbine Engines: Simulation of Flight Conditions in the Laboratory by Density Matching," International Journal of Turbo & Jet-Engines, Vol. 36, No. 2, 2019, pp. 157–173. https://doi.org/10.1515/tjj-2018-0021 CrossrefGoogle Scholar[22] Balcon N., Benard N., Lagmich Y., Boeuf J.-P., Touchard G. and Moreau E., "Positive and Negative Sawtooth Signals Applied to a DBD Plasma Actuator–Influence on the Electric Wind," Journal of Electrostatics, Vol. 67, Nos. 2–3, 2009, pp. 140–145. https://doi.org/10.1016/j.elstat.2009.01.019 CrossrefGoogle Scholar[23] Thomas F. O., Corke T. C., Iqbal M., Kozlov A. and Schatzman D., "Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control," AIAA Journal, Vol. 47, No. 9, 2009, pp. 2169–2178. https://doi.org/10.2514/1.41588 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 60, Number 6June 2022 CrossmarkInformationCopyright © 2022 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsActuatorsAerodynamicsAeronauticsAviationAviation RiskAviation SafetyAvionicsCompressor StallElectric HeatingFluid DynamicsHeating SystemHeating, Ventilating, and Air ConditioningIntegrated CircuitsSemiconductor DevicesThermal Control and ProtectionThermal EffectsThermal InsulationThermal MeasurementThermocouplesThermodynamicsThermophysics and Heat Transfer KeywordsPlasma ActuatorDielectric Barrier DischargeTemperature EffectsParticle Image VelocimetryAtmospheric ConditionsThermocouplesAero EngineBoundary Layer SeparationCharge Coupled DeviceComputational Fluid Dynamics SimulationAcknowledgmentsThe authors would like to thank the Natural Sciences and Engineering Research Council of Canada, whose funding under the Discovery Grants program was used for this research. The authors also gratefully acknowledge the support of Njuki W. Mureithi and Xin Gu for the particle image velocimetry system, and Philippe Massé for his help in setting up the experimental apparatus.PDF Received29 October 2021Accepted14 March 2022Published online27 April 2022

Récupéré en direct depuis OpenAlex et désinversé. Les résumés ne sont pas conservés dans cette base de données : les index inversés représentent 8,6 Go des 9,3 Go de texte de la base, et le serveur dispose de 13 Go libres.

Comment cette classification a été obtenuedéplier

Prédiction distillée sur la base complète

Imitation des enseignants

Ni prévalence calibrée, ni vérité terrain. Validation humaine à venir. Apprise à partir de 10 348 étiquettes directes de Codex et de 10 348 étiquettes directes de Gemma. Le mode candidate est l'union des têtes enseignantes seuillées; le consensus est leur intersection. Ces sorties portent le statut machine_predicted_unvalidated et ne sont ni des étiquettes humaines ni des étiquettes directes de modèles de pointe.

score de la tête « metaresearch » (Codex)0,000
score de la tête « metaresearch » (Gemma)0,000
Version: codex-gemma-dda1882f352aStatut de validation: machine_predicted_unvalidated
Catégories candidatesaucune
Catégories consensuellesaucune
DomaineSignal candidat: aucune · Signal consensuel: aucune
Devis d'étudeSignal candidat: Simulation ou modélisation · Signal consensuel: Simulation ou modélisation
GenreSignal candidat: Empirique · Signal consensuel: Empirique
Score de désaccord entre enseignants0,401
Score d'incertitude au seuil0,562

Scores Codex et Gemma par catégorie

CatégorieCodexGemma
Métarecherche0,0000,000
Méta-épidémiologie (sens strict)0,0000,000
Méta-épidémiologie (sens large)0,0000,000
Bibliométrie0,0000,000
Études des sciences et des technologies0,0000,000
Communication savante0,0000,000
Science ouverte0,0000,000
Intégrité de la recherche0,0000,001
Charge utile insuffisante (le modèle a refusé de juger)0,0000,000

Scores machine (provisoires)

Les deux têtes enseignantes du modèle étudiant, lues sur ce travail. Un score ordonne la base pour la relecture; il n'affirme jamais une catégorie, et le statut de validation accompagne chaque rangée tel quel.

Scores de référence d'un modèle non mature (critères de maturité non atteints, 7 itérations). Un score ordonne; il n'affirme jamais une catégorie.

Tête enseignante Opus0,002
Tête enseignante GPT0,165
Écart entre enseignants0,163 · la distance entre les deux têtes enseignantes sur ce seul travail
Statut de validationscore_only:v0-immature-baseline · tel quel depuis la passe de notation : score_only signifie que le nombre peut ordonner les travaux, et qu'aucune étiquette de catégorie n'en découle

Classification

machine, non validée

Prédiction automatique; un appel candidat d’une seule tête enseignante, pas un consensus.

Les modèles n’ont appliqué aucune catégorie : rien dans la taxonomie ne correspondait à ce travail.
Devis d'étudeSimulation ou modélisation
Domainenon disponible
GenreEmpirique

Le détail, modèle par modèle et score par score, se trouve en fin de page sous « Comment cette classification a été obtenue ».

En bref

Citations1
Publié2022
Routes d'admission3
Résumé présentoui

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