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Record W4224948513 · doi:10.2514/1.j061405

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

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

Bibliographic record

VenueAIAA Journal · 2022
Typearticle
Languageen
FieldEngineering
TopicPlasma and Flow Control in Aerodynamics
Canadian institutionsPolytechnique Montréal
FundersNatural Sciences and Engineering Research Council of Canada
KeywordsDielectric barrier dischargeAirfoilPlasma actuatorDielectricMaterials scienceEngineering physicsMechanical engineeringHumanitiesPhysicsEngineeringElectrical engineeringArtAerospace engineering

Abstract

fetched live from 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

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

How this classification was reachedexpand

Full frame distilled prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.

metaresearch head score (Codex)0.000
metaresearch head score (Gemma)0.000
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: Simulation or modeling
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.401
Threshold uncertainty score0.562

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0000.000
Research integrity0.0000.001
Insufficient payload (model declined to judge)0.0000.000

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.002
GPT teacher head0.165
Teacher spread0.163 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it

Classification

machine, unvalidated

Machine predicted; a candidate call from one teacher head, not a consensus.

The models applied no category: nothing in the taxonomy fit this work.
Study designSimulation or modeling
Domainnot available
GenreEmpirical

How this classification was reached, model by model and score by score, is at the end of the page under "How this classification was reached".

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Citations1
Published2022
Admission routes3
Has abstractyes

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