nach oben

Experiments in Fluids

Erschienen in:

01.06.2013 | Research Article

Control of oblique shock wave/boundary layer interactions using plasma actuators

verfasst von: N. Webb, C. Clifford, M. Samimy

Erschienen in: Experiments in Fluids | Ausgabe 6/2013

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config

KI-gestützte Suche

Aus

Abstract

Localized arc filament plasma actuators (LAFPAs) are used for shock wave/boundary layer interaction induced separation control in a Mach 2.3 flow. The boundary layer is fully turbulent with a Reynolds number based on the incompressible momentum thickness of 22,000 and shape factor of 1.37, and the impinging shock wave is generated by a 10° compression ramp. The LAFPAs are observed to have significant control authority over the interaction. The main effect is the displacement of the reflected shock and most of the interaction region upstream by approximately one boundary layer thickness (~5 mm). The initial goal of the control was to manipulate the low-frequency (St~0.03) unsteadiness associated with the interaction region. A detailed investigation of the effect of actuator placement, frequency, and duty cycle on the control authority indicates the actuators’ primary control mechanism is not the manipulation of low-frequency unsteadiness. Detailed measurements and analysis indicate that a modification to the boundary layer through heat addition by the actuators is the control mechanism, despite the extremely small power input of the actuators.

Vorheriger Artikel Particle image velocimetry measurements of flow field behind a circular square-edged orifice in a round pipe

Nächster Artikel Drop-on-demand for aqueous solutions of sodium alginate

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

über 102.000 Bücher
über 537 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Finance + Banking
Management + Führung
Marketing + Vertrieb
Maschinenbau + Werkstoffe
Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

über 67.000 Bücher
über 390 Zeitschriften

aus folgenden Fachgebieten:

Automobil + Motoren
Bauwesen + Immobilien
Business IT + Informatik
Elektrotechnik + Elektronik
Energie + Nachhaltigkeit
Maschinenbau + Werkstoffe

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Anderson B, Tinapple J, Surber L (2006) Optimal control of shock wave turbulent boundary layer interactions using micro-array actuation, 3rd AIAA Flow Control Conference p 3197

Andreopoulos J, Muck K (1987) Some new aspects of the shock-wave/boundary-layer interaction in compression-ramp flows. J Fluid Mech 180:405–428CrossRef

Babinsky H, Harvey J (2011) Shock wave-boundary-layer interactions. Cambridge University Press, New YorkMATHCrossRef

Babinsky H, Ogawa H (2008) SBLI control for wings and inlets. Shock Waves 18(2):89–96CrossRef

Babinsky H, Li Y, Ford C (2009) Microramp control of supersonic oblique shock-wave/boundary-layer interactions. AIAA J 47(3):668–675CrossRef

Babinsky H, Oorebeek J, Cottingham T (2013) Corner effects in reflecting oblique shock-wave/boundary-layer interactions, 51st AIAA Aerospace Sciences Meeting p 0859

Baruzzini D (2012) An industry perspective on the role of bleed in high-speed inlet design process, Private Communication

Baruzzini D, Domel N, Miller D (2012) Addressing corner interactions generated by oblique shock-waves in unswept right-angle corners and implications for high-speed inlets, 50th AIAA Aerospace Sciences Meeting: AIAA p 0275

Beresh S, Henfling J, Spillers R, Pruett B (2011) Very-large-scale coherent structures in the wall pressure field beneath a supersonic turbulent boundary layer, 49th AIAA Aerospace Sciences Meeting, p 746

Burton D, Babinsky H (2012) Corner separation effects for normal shock wave/turbulent boundary layer interactions in rectangular channels. J Fluid Mech 707:287–306CrossRef

Caraballo E, Webb N, Little J, Kim J-H, Samimy M (2009) Supersonic inlet flow control using plasma actuators, 47th AIAA Aerospace Sciences Meeting p 924

Dolling D (2001) Fifty years of shock-wave/boundary-layer interaction research: what next? AIAA J 39(8):1517–1531CrossRef

Dolling D, Brusniak L (1989) Separation shock motion in fin, cylinder, and compression ramp-induced turbulent interactions. AIAA J 27(6):734–742CrossRef

Dupont P, Haddad C, Debiève J-F (2006) Space and time organization in a shock-induced separated boundary layer. J Fluid Mech 559:255–277MATHCrossRef

Ganapathisubramani B, Clemens N, Dolling D (2009) Low-frequency dynamics of shock-induced separation in a compression ramp interaction. J Fluid Mech 636:397–425MATHCrossRef

Gefroh D, Loth E, Dutton C, McIlwain S (2002) Control of an oblique shock/boundary-layer interaction with aeroelastic mesoflaps. AIAA J 40(12):2456–2466CrossRef

Hahn C, Kearney-Fischer M, Samimy M (2011) On factors influencing arc filament plasma actuator performance in control of high speed jets. Exp Fluids 37:5

Jaunet V, Debiève J-F, Dupont P (2012) Experimental investigation of an oblique shock reflection with separation over a heated wall, 50th AIAA Aerospace Sciences Meeting AIAA p 1095

Kalra C, Zaidi S, Miles R, Macheret S (2011) Shockwave-turbulent boundary layer interaction control using magnetically driven surface discharges. Exp Fluids 50:547–559CrossRef

Lee S, Goettke M, Loth E, Tinapple J, Benek J (2010a) Microramps upstream of an oblique-shock/boundary-layer interaction. AIAA J 48(1):104–118CrossRef

Lee S, Loth E, Babinsky H (2010) Normal shock boundary layer control with various vortex generator geometries, AIAA 5th Flow Control Conference p 4254

Little J, Takashima K, Nishihara M, Adamovich I, Samimy M (2012) Separation control with nanosecond-pulse-driven dielectric barrier discharge plasma actuators. AIAA J 50(2):350–365CrossRef

Maise G, McDonald H (1968) Mixing length and kinematic eddy viscosity in a compressible boundary layer. AIAA J 6(1):73–80CrossRef

Narayanaswamy V (2010) Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control. Dissertation, University of Texas at Austin

Narayanaswamy V, Raja L, Clemens N (2012) Control of a shock/boundary layer interaction by using a pulsed-plasma jet actuator. AIAA J 50(1):246–249CrossRef

Piponniau S, Dussauge J, Debieve J, Dupont P (2009) A simple model for low-frequency unsteadiness in shock-induced separation. J Fluid Mech 629:87–108MATHCrossRef

Pirozzoli S, Grasso F (2006) Direct numerical simulation of impinging shock wave/turbulent boundary layer interaction at M = 2.25. Phys Fluids A 18:1–17

Rethmel C, Little J, Takashima K, Sinha A, Adamovich I, Samimy M (2011) Flow separation control using nanosecond pulse driven DBD plasma actuators. Int J Flow Control 3(4):213–232CrossRef

Samimy M, Kim J-H, Kastner J, Adamovich I, Utkin Y (2007a) Active control of high-speed and high-Reynolds-number jets using plasma actuators. J Fluid Mech 578(1):305–330MATHCrossRef

Samimy M, Kim J-H, Kastner J, Adamovich I, Utkin Y (2007b) Active control of a mach 0.9 jet for noise mitigation using plasma actuators. AIAA J 45(4):890–901CrossRef

Samimy M, Kim J-H, Kearney-Fischer M, Sinha A (2010) Acoustic and flow fields of an excited high Reynolds number axisymmetric supersonic jet. J Fluid Mech 656:507–529MATHCrossRef

Samimy M, Kearney-Fischer M, Kim J-H, Sinha A (2012) High-speed and high-Reynolds-number jet control using localized arc filament plasma actuators. J Propul Power 28:2

Shahneh A, Motallebi F (2009) Effect of submerged vortex generators on shock-induced separation in transonic flow. J Aircraft 46(3):856–863CrossRef

Sinha A, Kim K, Kim J-H, Serrani A, Samimy M (2010) Extremizing feedback control of a high-speed and high Reynolds number jet. AIAA J 48(2):387–399CrossRef

Solomon J, Kumar R, Alvi F (2010) High-bandwidth pulsed microactuators for high-speed flow control. AIAA J 48(10):2386–2396CrossRef

Souverein L, Debiève J-F (2010) Effect of air jet vortex generators on a shock wave boundary layer interaction. Exp Fluids 49:1053–1064CrossRef

Souverein L, Bakker P, Dupont P (2013) A scaling analysis for turbulent shock-wave/boundary-layer interactions. J Fluid Mech 714:505–535MathSciNetCrossRef

Syberg J, Koncsek J (1976) Experimental evaluation of an analytically derived bleed system for a supersonic inlet. J Aircraft 13(10):792–797CrossRef

Titchener N, Babinsky H, Loth E (2012) Can fundamental shock-wave/boundary-layer interaction research be relevant to inlet aerodynamics?, 50th AIAA Aerospace Sciences Meeting, AIAA p 0017

Touber E, Sandham N (2009) Large-eddy simulation of low-frequency unsteadiness in a turbulent shock-induced separation bubble. Theoret Comput Fluid Dyn 23:79–107MATHCrossRef

Touber E, Sandham N (2011) Low-order stochastic modelling of low-frequency motions in reflected shock-wave/boundary-layer interactions. J Fluid Mech 671:417–465MATHCrossRef

Utkin Y, Keshav S, Kim J-H, Kastner J, Adamovich I, Samimy M (2007) Development and use of localized arc filament plasma actuators for high-speed flow control. J Phys D Appl Phys 40(3):685–694CrossRef

Webb N (2013) Control of a shock wave-boundary layer interaction using localized arc filament plasma actuators, Dissertation. The Ohio State University

Webb N, Clifford C, Samimy M (2011) Preliminary results on shock wave/boundary layer interaction control using localized arc filament plasma actuators, 41st AIAA Fluid Dynamics Conference p 3426

Yugulis K, Gregory J, Samimy M (2013) Control of high subsonic cavity flow using plasma actuators, 51st AIAA Aerospace Sciences Meeting p 0679

Titel: Control of oblique shock wave/boundary layer interactions using plasma actuators
verfasst von: N. Webb
C. Clifford
M. Samimy
Publikationsdatum: 01.06.2013
Verlag: Springer Berlin Heidelberg
Erschienen in: Experiments in Fluids / Ausgabe 6/2013
Print ISSN: 0723-4864
Elektronische ISSN: 1432-1114
DOI: https://doi.org/10.1007/s00348-013-1545-z

Premium Partner

Marktübersichten

Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.

Zur Marktübersicht

Springer Professional

Abstract

Bitte loggen Sie sich ein, um Zugang zu Ihrer Lizenz zu erhalten.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Springer Professional "Technik"

Weitere Artikel der Ausgabe 6/2013

Single- and dual-band collection toluene PLIF thermometry in supersonic flows

Comparison of experiments and simulations for zero pressure gradient turbulent boundary layers at moderate Reynolds numbers

Experimental study of the internal flow structures inside a fluidic oscillator

Measurement of width and intensity of particle streaks in turbulent flows

Spatially resolved measurements in a liquid metal flow with Lorentz force velocimetry

Three-dimensional flow in a lid-driven cavity with width-to-height ratio of 1.6

Premium Partner

Marktübersichten