Closed-loop control of a turbulent wake by Dielectric Barrier Discharge (DBD)
|
|
- Lisa Tucker
- 5 years ago
- Views:
Transcription
1 Journées du GDR "Controle Des Décollements", Ecole centrale, Lyon, 28/11/2016 Closed-loop control of a turbulent wake by Dielectric Barrier Discharge (DBD) V. Parezanovic, Y. Bury and L. Joly ISAE-SUPAERO, Toulouse 1
2 In the context of project «CARPE»... Project motivation: - CARPE: Robust control of flow behind a thick plate (Contrôle Actif Robuste d écoulement de Plaque Epaisse) - Reduction of drag by closed-loop control - Control of a bluff cylinder wake, ie. von Karman vortex street - Closing the loop to obtain robustness Experimental study goals: - Working closed-loop control prototype - Detailed flow study (actuator physics, wake dynamics, different configurations, etc...) - Implementation of a model-based controller (with IMT, Toulouse)
3 In the context of project «CARPE»... Project motivation: - CARPE: Robust control of flow behind a thick plate - Reduction of drag by closed-loop control - Control of a bluff cylinder wake, ie. von Karman vortex street - Closing the loop to obtain robustness Experimental study goals: - Working closed-loop control prototype - Detailed flow study (actuator physics, wake dynamics, different configurations, etc...) - Implementation of a model-based controller (with IMT, Toulouse)
4 Wake stabilization at low Re Steady disturbance control (small control cylinder) Complete vortex shedding extinction at Re=46 with D/d=10 P. J. Strykowski and K. R. Sreenivasan, (1990) 4
5 Profile drag of a 2D bluff body Parezanovic, V. & Cadot, O. (2012). Experimental sensitivity analysis of the global properties of a two-dimensional turbulent wake. Journal of Fluid Mechanics, 693,
6 Closed-loop control Feedback control / direct wake control / primary instability / synchronisation Pastoor, M., Henning, L., Noack, B. R., King, R., & Tadmor, G. (2008). Feedback shear layer control for bluff body drag reduction. Journal of Fluid Mechanics, 608(7), Stalnov, O., Fono, I., & Seifert, A. (2011). Closed-loop bluff-body wake stabilization via fluidic excitation. Theoretical and Computational Fluid Dynamics, 25(1-4),
7 Control of the secondary wake instability Active or passive / steady perturbation / secondary instability / reducing 2D flow ordering Park, H., Lee, D., Jeon, W. P., Hahn, S., Kim, J., Kim, J.,... & Choi, H. (2006). Drag reduction in flow over a twodimensional bluff body with a blunt trailing edge using a new passive device. Journal of Fluid Mechanics, 563, Naghib-Lahouti, A., Hangan, H., & Lavoie, P. (2015). Distributed forcing flow control in the wake of a blunt trailing edge profiled body using plasma actuators. Physics of Fluids (1994-present), 27(3),
8 Overview of control strategies Type of control Open-loop control Closed-loop control Actuation Steady perturbation Time-dependent perturbation (De)synchronisation shear modification? vortex dislocation Target Primary instability (von Karman v.s.) Secondary instability (streamwise structures)
9 Model-free vs. model-based control? Natural flow pressure measurements (courtesy of A. Debien, ONERA) Raw signal Filtered signal Phase Model-free feedback control (similar to Stalnov et al.) can be implemented Linear system identification methods in numerical simulations (low Re numbers) Dahan, J. A., Morgans, A. S., & Lardeau, S. (2012). Feedback control for form-drag reduction on a bluff body with a blunt trailing edge. Journal of Fluid Mechanics, 704, Flinois, T., Morgans, A. S. (2016) Feedback control of unstable flows: a direct modelling approach using the Eigensystem Realisation Algorithm. Journal of Fluid Mechanics, 793,
10 Design of the CARPE experiment Digital mock-up (by S. Prothin, ISAE) DBD actuator Pro: high flexibility in position, orientation and controlability Con: proximity of sensors and actuators, EM interference
11 Boundary layer and the global mode frequency y (mm) U (m/s) U 0 (m/s) Re(U 0, D) y (U max )(mm) delta (m) theta (m) Re (theta) H U 0 (m/s) f VKS (Hz) St t (ms)
12 Dielectric Barrier Discharge (DBD) actuator Top-down view of the model Sensors (mounted inside) DBD properties: Electrodes f c = 2.4 khz u peak = 10-20kV i = 24mA U jet 2-4 m/s Strioscopic imagery of the DBD jet propagation in a still environment
13 Control loop design Sensor signal: real time pressure measurements + lowpass filtering P1 g (t) - actuation p 1 p 0 Head pressure sensor p 3 p 2 Pressure sensors on the base P2 Proportional control: g(t+δt) = C s(t) Objective function: C pb = p 3 / p 0
14 Control loop design Sensor signal: real time pressure measurements + lowpass filtering P1 g (t) - actuation p 1 L b p 0 Head pressure sensor p 3 C pb C d p 2 Pressure sensors on the base P2
15 Sensor delay Δt s = 0 Δt s = 3 ms
16 Closed-loop control (I) Δt = 0, ΔΦ (p2) 0 Δt = 25 ms, ΔΦ (p2) = 360 U 0 = 3.5 m/s Re 4900 Actuation (0=ON) (1 - C pb /C pbn )*100 P1 (Pa) ΔΦ (p2) 0 ΔΦ (p1) 0 ΔΦ (p1) = 180 U 0 = 5.1 m/s Re 7000
17 Future tasks Detailed flow study in a large scale setup: - Large scale model easier to integrate with the sensors and the DBD actuator - SABRE wind tunnel facility enables a lower Re number study (similar to numerical simulations) - Time resolved PIV for elucidating on the synchronization mechanism - Close-in PIV to resolve the DBD actuator dynamics vs the boundary/shear layer - Alternative actuator location (at the base, blowing perpendicular to the separated shear layer) - Implementation of a linear model-based controller (partially designed using low Re number simulations from IMT)
18 Thank you!
Drag reduction by closed-loop control of a separated flow over a bluff body with a blunt trailing edge
Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference 25 Seville, Spain, December 12-15, 25 MoA15.1 Drag reduction by closed-loop control of a separated flow
More informationReducing the pressure drag of a D-shaped bluff body using linear feedback control
Theor. Comput. Fluid Dyn. DOI.7/s6-7-4-6 ORIGINAL ARTICLE L. Dalla Longa A. S. Morgans J. A. Dahan Reducing the pressure drag of a D-shaped bluff body using linear feedback control Received: 9 February
More informationForcing the shear layer of a backward-facing step flow
Forcing the shear layer of a backward-facing step flow using DBD plasma actuator J.-L. Aider* T. Duriez* J. E. Wesfreid* G. Artana *Laboratoire PMMH UMR7636 CNRS ESPCI - France Laboratorio de FluidoDynamica
More informationAdvanced Engine Noise Control Based on Plasma Actuators. Franck Cléro, Onera Victor Kopiev, TsAGI
Advanced Engine Noise Control Based on Plasma Actuators Franck Cléro, Onera Victor Kopiev, TsAGI Fan Soufflante Compresseur Compressor Combustion Combustinr Jet Turbine Turbine Aerodynamique Airframe noise
More informationVortex Induced Vibrations
Vortex Induced Vibrations By: Abhiroop Jayanthi Indian Institute of Technology, Delhi Some Questions! What is VIV? What are the details of a steady approach flow past a stationary cylinder? How and why
More informationEFFECT OF BOUNDARY LAYER THICKNESS AND PASSIVE VORTEX GENERATORS ON THE WAKE OF A BLUNT TRAILING EDGE PROFILED BODY. Wenyi Zhao
EFFECT OF BOUNDARY LAYER THICKNESS AND PASSIVE VORTEX GENERATORS ON THE WAKE OF A BLUNT TRAILING EDGE PROFILED BODY by Wenyi Zhao A thesis submitted in conformity with the requirements for the degree of
More informationControl of Flow over a Bluff Body
Annu. Rev. Fluid Mech. 2008 40 1056-8700/97/0610-00 Control of Flow over a Bluff Body Haecheon Choi 1,2, Woo-Pyung Jeon 1 and Jinsung Kim 1 1 School of Mechanical and Aerospace Engineering, Seoul National
More informationA Pair of Large-incidence-angle Cylinders in Cross-flow with the Upstream One Subjected to a Transverse Harmonic Oscillation
Proceedings of the 2010 International Conference on Industrial Engineering and Operations Management Dhaka, Bangladesh, January 9 10, 2010 A Pair of Large-incidence-angle Cylinders in Cross-flow with the
More informationPERTURBING SHEAR LAYERS IN A TURBULENT WAKE
PERTURBING SHEAR LAYERS IN A TURBULENT WAKE Diogo Barros, Jacques Borée, Andreas Spohn Institut Pprime, UPR-3346 CNRS - ISAE-ENSMA - Université de Poitiers Futuroscope Chasseneuil, France. diogo.barros@ensma.fr
More informationPROPERTIES OF THE FLOW AROUND TWO ROTATING CIRCULAR CYLINDERS IN SIDE-BY-SIDE ARRANGEMENT WITH DIFFERENT ROTATION TYPES
THERMAL SCIENCE, Year, Vol. 8, No. 5, pp. 87-9 87 PROPERTIES OF THE FLOW AROUND TWO ROTATING CIRCULAR CYLINDERS IN SIDE-BY-SIDE ARRANGEMENT WITH DIFFERENT ROTATION TYPES by Cheng-Xu TU, a,b Fu-Bin BAO
More informationExperimental Aerodynamics. Experimental Aerodynamics
Lecture 3: Vortex shedding and buffeting G. Dimitriadis Buffeting! All structures exposed to a wind have the tendency to vibrate.! These vibrations are normally of small amplitude and have stochastic character!
More informationAEROACOUSTIC INVESTIGATION OF THE EFFECT OF A DETACHED FLAT PLATE ON THE NOISE FROM A SQUARE CYLINDER
Abstract AEROACOUSTIC INVESTIGATION OF THE EFFECT OF A DETACHED FLAT PLATE ON THE NOISE FROM A SQUARE CYLINDER Aniket D. Jagtap 1, Ric Porteous 1, Akhilesh Mimani 1 and Con Doolan 2 1 School of Mechanical
More informationWake flow stabilization with DBD plasma actuators for low Re numbers
Wake flow stabilization with DBD plasma actuators for low Re numbers Juan D Adamo, Roberto Sosa, Marcos Barceló, Guillermo Artana Laboratorio de Fluidodinámica, Facultad de Ingeniería. Universidad de Buenos
More informationAerodynamic Characteristics of Flow over Circular Cylinders with Patterned Surface
Aerodynamic Characteristics of Flow over Circular Cylinders with Patterned Surface U. Butt and C. Egbers Abstract Flow over circular cylinders with patterned surfaces is investigated and discussed taking
More informationClosed-loop turbulence control using machine learning Stop thinking and let your PC and experiment do the hard work!
Closed-loop turbulence control using machine learning Stop thinking and let your PC and experiment do the hard work! B. Noack 3, T. Duriez 1,3, L. Cordier 3, K. von Krbek 3, E. Kaiser 3,4, V. Parezanovic
More informationCirculation control using surface plasma actuators for aerodynamic load alleviation on wind turbine airfoils
Circulation control using surface plasma actuators for aerodynamic load alleviation on wind turbine airfoils P. JOSEPH, A. LEROY, S. BALERIOLA, D. NELSON-GRUEL, Y. HAIDOUS, S. LOYER, P. DEVINANT, S. AUBRUN
More informationActive Control of Turbulence and Fluid- Structure Interactions
Bonjour! Active Control of Turbulence and Fluid- Structure Interactions Yu Zhou Institute for Turbulence-Noise-Vibration Interaction and Control Shenzhen Graduate School, Harbin Institute of Technology
More informationFLOW CONTROL USING DBD PLASMA ON BACKWARD-FACING STEP
28 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES FLOW CONTROL USING DBD PLASMA ON BACKWARD-FACING STEP Jiwoon Song* * Department of Mechanical Engineering, Yonsei University, 120-749, Korea dolguard@yonsei.ac.kr
More informationAnalysis of the Effects of SD Plasma on Aerodynamic Drag Reduction of a High-speed Train
J Electr Eng Technol Vol. 9, No.?: 742-?, 2014 http://dx.doi.org/10.5370/jeet.2014.9.5.742 ISSN(Print) 1975-0102 ISSN(Online) 2093-7423 Analysis of the Effects of SD Plasma on Aerodynamic Drag Reduction
More informationBluff Body Flow Separation Control using Surface Dielectric Barrier Discharges
45th AIAA Aerospace Sciences Meeting and Exhibit 8-45th 11 January AIAA Aerospace 2007, Reno, Sciences Nevada Meeting and Exhibit 8 11 January 2007, Reno, Nevada AIAA 2007-939 Bluff Body Flow Separation
More informationExperimental Study of Flow Control Over an Ahmed Body Using Plasma Actuator
Mechanics and Mechanical Engineering Vol. 22, No. 1 (2018) 239 251 c Lodz University of Technology Experimental Study of Flow Control Over an Ahmed Body Using Plasma Actuator S. Shadmani S. M. Mousavi
More informationVortex shedding from slender surface mounted pyramids
Vortex shedding from slender surface mounted pyramids M. J. Morrison 1, R. J. Martinuzzi 3, E. Savory 1, G. A. Kopp 2 1 Department of Mechanical and Materials Engineering, University of Western Ontario,
More informationARTIFICIAL TURBULIZATION OF THE SUPERSONIC BOUNDARY LAYER BY DIELECTRIC BARRIER DISCHARGE
ARTIFICIAL TURBULIZATION OF THE SUPERSONIC BOUNDARY LAYER BY DIELECTRIC BARRIER DISCHARGE P.А. Polivanov, A.А. Sidorenko & A.А. Maslov Khristianovich Institute of Theoretical and Applied Mechanics SB RAS
More informationEFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIRFOIL
EFFECTIVE PLASMA BUFFET AND DRAG CONTROL FOR LAMINAR TRANSONIC AIRFOIL Pavel A. Polivanov*, Andrey A. Sidorenko* * Khristianovich Institute of Theoretical and Applied Mechanics SB RAS 630090, Institutskaya,
More informationAvailable online at ScienceDirect. Procedia IUTAM 14 (2015 ) IUTAM ABCM Symposium on Laminar Turbulent Transition
Available online at www.sciencedirect.com ScienceDirect Procedia IUTAM 14 (2015 ) 115 121 IUTAM ABCM Symposium on Laminar Turbulent Transition Stabilisation of the absolute instability of a flow past a
More informationInvestigation of fluid flow around a cylinder with EHD actuation on inclined plates behind the cylinder
Investigation of fluid flow around a cylinder with EHD actuation on inclined plates behind the cylinder S. Reza-zadeh Department of Mechanical Engineering, Hakim Sabzevari University (HSU), Sabzevar, Iran
More informationModelling and feedback control of turbulent coherent structures for bluff body drag reduction
th International Symposium on Turbulence and Shear Flow Phenomena (TSFP), Chicago, USA, July, 27 Modelling and feedback control of turbulent coherent structures for bluff body drag reduction Rowan D. Brackston
More informationFlow Control. Jean-Pierre Richard. joint work with
Flow Control Jean-Pierre Richard http://chercheurs.lille.inria.fr/~jrichard/ joint work with Maxime Feingesicht (Department of Aerospace Engineering, The University of Michigan) Andrey Polyakov (Inria,
More informationCOMPUTATIONAL STUDY OF SEPARATION CONTROL MECHANISM WITH THE IMAGINARY BODY FORCE ADDED TO THE FLOWS OVER AN AIRFOIL
COMPUTATIONAL STUDY OF SEPARATION CONTROL MECHANISM WITH THE IMAGINARY BODY FORCE ADDED TO THE FLOWS OVER AN AIRFOIL Kengo Asada 1 and Kozo Fujii 2 ABSTRACT The effects of body force distribution on the
More informationNumerical Investigation of the Fluid Flow around and Past a Circular Cylinder by Ansys Simulation
, pp.49-58 http://dx.doi.org/10.1457/ijast.016.9.06 Numerical Investigation of the Fluid Flow around and Past a Circular Cylinder by Ansys Simulation Mojtaba Daneshi Department of Mechanical Engineering,
More informationApplied Thermal and Fluid Engineering. Energy Engineering (Thermal Engineering Laboratory)
Applied Thermal and Fluid Engineering Energy Engineering (Thermal Engineering Laboratory) Professor Assoc. Professor Hajime Nakamura Shunsuke Yamada Outline of Research In our laboratory, we have been
More informationElectrohydrodynamic phenomena in atmospheric discharges : application to airflow control by plasma actuators
Proc. 216 Electrostatics Joint Conference 1 Electrohydrodynamic phenomena in atmospheric discharges : application to airflow control by plasma actuators Eric Moreau, Nicolas Benard University of Poitiers,
More informationActive drag reduction in a turbulent boundary layer based on plasma-actuatorgenerated streamwise vortices
June 30 - July 3, 015 Melbourne, Australia 9 9A-5 Active drag reduction in a turbulent boundary layer based on plasma-actuatorgenerated streamwise vortices Chi Wai Wong, Yu Zhou, Yinzhe Li and Yupeng Li
More informationTHE EFFECT OF SAMPLE SIZE, TURBULENCE INTENSITY AND THE VELOCITY FIELD ON THE EXPERIMENTAL ACCURACY OF ENSEMBLE AVERAGED PIV MEASUREMENTS
4th International Symposium on Particle Image Velocimetry Göttingen, Germany, September 7-9, 00 PIV 0 Paper 096 THE EFFECT OF SAMPLE SIZE, TURBULECE ITESITY AD THE VELOCITY FIELD O THE EXPERIMETAL ACCURACY
More informationOn the Frequency Scaling of the Forced Flow Above a Low Aspect Ratio Wing
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 09-12 January 2012, Nashville, Tennessee AIAA 2012-0317 On the Frequency Scaling of the Forced Flow Above
More informationLAMINAR-TURBULENT TRANSITION CONTROL BY DIELECTRIC BARRIER DISCHARGE. THEORY AND EXPERIMENT
LAMINAR-TURBULENT TRANSITION CONTROL BY DIELECTRIC BARRIER DISCHARGE. THEORY AND EXPERIMENT M.V. Ustinov*, A.A. Uspensky*, A. Yu. Urusov*, D.A. Rusianov* *Central Aerohydrodynamic Institute (TsAGI) Keywords:
More informationLARGE EDDY SIMULATION AND FLOW CONTROL OVER A 25 RAMP MODEL
LARGE EDDY SIMULATION AND FLOW CONTROL OVER A 25 RAMP MODEL 09/11/2017 Paolo Casco Stephie Edwige Philippe Gilotte Iraj Mortazavi LES and flow control over a 25 ramp model : context 2 Context Validation
More informationACTIVE SEPARATION CONTROL PROCESS OVER A SHARP EDGE RAMP
June 30 - July 3, 2015 Melbourne, Australia 9 3D-1 ACTIVE SEPARATION CONTROL PROCESS OVER A SHARP EDGE RAMP Antoine Debien 8 rue Léonard de Vinci antoine.debien@univ-orleans.fr Sandrine Aubrun sandrine.aubrun@univ-orleans.fr
More informationCharacterisation of a square back Ahmed body near wake flow
1ème Congrès Français de Mécanique Bordeaux, 6 au 3 août 13 Characterisation of a square back Ahmed body near wake flow A. Lahaye a,b, A. Leroy a, A. Kourta a a. PRISME Laboratory, University of Orléans
More informationComputational characterization of vortexes generated by low-profile Vortex Generators
2017 Pamplona-Iruña, 26-28 April 2017 Computational characterization of vortexes generated by low-profile Vortex Generators Iosu Ibarra Udaeta, Iñigo Errasti Arrieta, Unai Fernández- Gamiz, Ekaitz Zulueta,
More informationInfluence of After Body Shape on the Performance of Blunt Shaped Bodies as Vortex Shedders
Influence of After Body Shape on the Performance of Blunt Shaped Bodies as Vortex Shedders Lavish Ordia, A. Venugopal, Amit Agrawal, S. V. Prabhu Abstract The present study explores flow visualization
More informationDrag Reduction in Flow Separation. Using Plasma Actuator in a Cylinder Model
Drag Reduction in Flow Separation Using Plasma Actuator in a Cylinder Model Harinaldi1, a, Budiarso1, b, James Julian2, c,*, Andika. W.S2, d 1 Mechanical Engineering Department, Faculty of Engineering
More informationSalient and smooth edge ramps inducing turbulent boundary layer separation: flow characterization for control perspective
Salient and smooth edge ramps inducing turbulent boundary layer separation: flow characterization for control perspective A. Debien, S. Aubrun, N. Mazellier, A. Kourta Projet ANR- 11-BS09-018 SePaCoDe
More informationCOURSE ON VEHICLE AERODYNAMICS Prof. Tamás Lajos University of Rome La Sapienza 1999
COURSE ON VEHICLE AERODYNAMICS Prof. Tamás Lajos University of Rome La Sapienza 1999 1. Introduction Subject of the course: basics of vehicle aerodynamics ground vehicle aerodynamics examples in car, bus,
More informationAerodynamic modification of flow over bluff objects by plasma actuation
Experiments in Fluids (2006) 41: 479 486 DOI 10.1007/s00348-006-0175-0 RESEARCH ARTICLE Y. Sung Æ W. Kim Æ M. G. Mungal Æ M. A. Cappelli Aerodynamic modification of flow over bluff objects by plasma actuation
More informationDépartement AUTOMATIQUE
Bombardier Toyota Railway industry 10 000 employees 1 st European region for railway 4 International manufacturers leaders 1 Billion euros sales revenue LAMIH Alstom MCA Automobile industry 36 000 employees
More informationSelf-Excited Vibration in Hydraulic Ball Check Valve
Self-Excited Vibration in Hydraulic Ball Check Valve L. Grinis, V. Haslavsky, U. Tzadka Abstract This paper describes an experimental, theoretical model and numerical study of concentrated vortex flow
More informationFlow Control around Bluff Bodies by Attached Permeable Plates
Flow Control around Bluff Bodies by Attached Permeable Plates G. M. Ozkan, H. Akilli Abstract The aim of present study is to control the unsteady flow structure downstream of a circular cylinder by use
More informationTIME-AVERAGED PHENOMENOLOGICAL INVESTIGATION OF A WAKE BEHIND A BLUFF BODY
BBAA VI International Colloquium on: Bluff Bodies Aerodynamics & Applications Milano, Italy, July, 20 24 2008 TIME-AVERAGED PHENOMENOLOGICAL INVESTIGATION OF A WAKE BEHIND A BLUFF BODY G.M.R. Van Raemdonck
More informationThis is an author-deposited version published in: Eprints ID: 9937
Open Archive Toulouse Archive Ouverte (OATAO) OATAO is an open access repository that collects the work of Toulouse researchers and makes it freely available over the web where possible. This is an author-deposited
More informationMODELING OF PLASMA ACTUATOR AND ITS EFFECT ON FLOW FIELD AROUND RECTANGULAR CYLINDER
Indian J.Sci.Res.1(2) : 803-814, 2014 ISSN : 0976-2876 (Print) ISSN : 2250-0138(Online) MODELING OF PLASMA ACTUATOR AND ITS EFFECT ON FLOW FIELD AROUND RECTANGULAR CYLINDER SAEED KAVOUSFAR a, HOSSEIN MAHDAVY-MOGHADDAM
More informationNumerical and Experimental Investigation of the Flow-Induced Noise of a Wall Mounted Airfoil
Numerical and Experimental Investigation of the Flow-Induced Noise of a Wall Mounted Airfoil Paul Croaker, Danielle Moreau, Manuj Awasthi, Mahmoud Karimi, Con Doolan, Nicole Kessissoglou School of Mechanical
More informationElectric Field Measurements in Atmospheric Pressure Electric Discharges
70 th Gaseous Electronics Conference Pittsburgh, PA, November 6-10, 2017 Electric Field Measurements in Atmospheric Pressure Electric Discharges M. Simeni Simeni, B.M. Goldberg, E. Baratte, C. Zhang, K.
More informationInteraction of fluidic actuators and a flat plate boundary layer: experiments and first results
Interaction of fluidic actuators and a flat plate boundary layer: experiments and first results Célestin OTT PhD student - 2 nd year ONERA Lille, LAMIH Valenciennes Thesis director: Laurent KEIRSBULCK
More informationCamila Chovet Laurent Keirsbulck Bernd. R. Noack
Camila Chovet Laurent Keirsbulck Bernd. R. Noack Marc Lippert Jean-Marc Foucaut Lyon, 2016 November 28 INTRO 1 Bombardier Toyota LAMIH Alstom MCA PSA Railway industry 10 000 employees 1 st European region
More informationNumerical Simulation of Flow Separation Control using Multiple DBD Plasma Actuators
Journal of Applied Fluid Mechanics, Vol. 9, No. 4, pp. 1865-1875, 2016. Available online at www.jafmonline.net, ISSN 1735-3572, EISSN 1735-3645. DOI: 10.18869/acadpub.jafm.68.235.25325 Numerical Simulation
More informationTurbulent separated shear flow control by surface plasma actuator Experimental optimization by genetic algorithm approach
1 Turbulent separated shear flow control by surface plasma actuator Experimental optimization by genetic algorithm approach N. Benard *1, J. Pons-Prats 2, J. Periaux 2,3, G. Bugeda 2,3, P. Braud 1, J.P.
More informationApplication of wall forcing methods in a turbulent channel flow using Incompact3d
Application of wall forcing methods in a turbulent channel flow using Incompact3d S. Khosh Aghdam Department of Mechanical Engineering - University of Sheffield 1 Flow control 2 Drag reduction 3 Maths
More informationFLOW MEASUREMENT. INC 102 Fundamental of Instrumentation and Process Control 2/2560
FLOW MEASUREMENT INC 102 Fundamental of Instrumentation and Process Control 2/2560 TABLE OF CONTENTS A. INTRODUCTION B. LOCAL FLOW MEASUREMENT B.1 Particle Image Velocimetry (PIV) B.2 Laser doppler anemometry
More informationBurst Frequency effect of DBD Plasma actuator on the control of separated flow over an airfoil
24 Burst Frequency effect of DBD Plasma actuator on the control of separated flow over an airfoil,, 252-5210 3-1-1, asada@flab.isas.jaxa.jp, ISAS/JAXA, 252-5210 3-1-1, fujii@flab.isas.jaxa.jp Kengo Asada,
More informationFeedback control of particle dispersion in bluff body wakes
INT. J. CONTROL,, VOL. 77, NO. 11, 11 118 Feedback control of particle dispersion in bluff body wakes OLE MORTEN AAMOy* and MIROSLAV KRSTIC z We address the problem of imposing particle dispersion, or
More informationEXPERIMENTS OF CLOSED-LOOP FLOW CONTROL FOR LAMINAR BOUNDARY LAYERS
Fourth International Symposium on Physics of Fluids (ISPF4) International Journal of Modern Physics: Conference Series Vol. 19 (212) 242 249 World Scientific Publishing Company DOI: 1.1142/S211945128811
More informationSide-View Mirror Vibrations Induced Aerodynamically by Separating Vortices
Open Journal of Fluid Dynamics, 2016, 6, 42-56 Published Online March 2016 in SciRes. http://www.scirp.org/journal/ojfd http://dx.doi.org/10.4236/ojfd.2016.61004 Side-View Mirror Vibrations Induced Aerodynamically
More informationinter.noise 2000 The 29th International Congress and Exhibition on Noise Control Engineering August 2000, Nice, FRANCE
Copyright SFA - InterNoise 2000 1 inter.noise 2000 The 29th International Congress and Exhibition on Noise Control Engineering 27-30 August 2000, Nice, FRANCE I-INCE Classification: 1.0 NOZZLE DESIGN EFFECT
More informationFlow disturbance due to presence of the vane anemometer
Journal of Physics: Conference Series OPEN ACCESS Flow disturbance due to presence of the vane anemometer To cite this article: M Bujalski et al 24 J. Phys.: Conf. Ser. 53 245 View the article online for
More informationTurbulence Modeling Applied to Flow over a Hydraulic Ball Check Valve
Engineering, 2,, 68-6 http://dx.doi.org/.426/eng.2.88 Published Online August 2 (http://www.scirp.org/journal/eng) Turbulence Modeling Applied to Flow over a Hydraulic Ball Check Valve Leonid Grinis, Vitaly
More informationAn Experimental Study Of An Electroaerodynamic Actuator
Copyright 21 Tech Science Press FDMP, vol.6, no.4, pp.49-418, 21 An Experimental Study Of An Electroaerodynamic Actuator R. Mestiri 1, R. Hadaji 1 and S. Ben Nasrallah 1 Abstract: The electroaerodynamic
More informationFINAL REPORT. Office of Naval Research. entitled. Anatol Roshko Theodore Von Karman Professor of Aeronautics
to F11 F rnpv FINAL REPORT 4to Office of Naval Research on Contract No. N00014-85-C-0646 Work Unit No. 4328-434 entitled STRUCTURE AND MIXING IN TURBULENT SHEAR FLOWS 1 July 1985-31 October 1988 Anatol
More informationStability, cyclone-anticyclone asymmetry and frequency selection in rotating shallow-water wakes
Stability, cyclone-anticyclone asymmetry and frequency selection in rotating shallow-water wakes T. Dubos 1, G. Perret 1,2, A. Stegner 1, J.-M. Chomaz 3 and M. Farge 1 1 IPSL/Laboratoire de Meteorologie
More informationFlow control. Flow Instability (and control) Vortex Instabilities
Flow control Flow Instability (and control) Tim Colonius CDS 101 Friday, Oct 15, 2004 Many control problems contain fluid systems as components. Dashpot in mass-spring-damper systems HVAC system that thermostat
More informationSHEAR-LAYER MANIPULATION OF BACKWARD-FACING STEP FLOW WITH FORCING: A NUMERICAL STUDY
SHEAR-LAYER MANIPULATION OF BACKWARD-FACING STEP FLOW WITH FORCING: A NUMERICAL STUDY Shia-Hui Peng Swedish Defence Research Agency, FOI, Sweden peng@foi.se 1 Introduction By means of experimental and
More informationMeasuring the Vortex-Shedding Frequency Behind Staggered Cylinders in Cross-Flow
Santa Clara University Scholar Commons Mechanical Engineering Master's Theses Engineering Master's Theses 8-2018 Measuring the Vortex-Shedding Frequency Behind Staggered Cylinders in Cross-Flow Christopher
More information(a) Re=150 (Spanwise domain: 8D) (b) Re=200 (Spanwise domain: 8D) (c) Re=300 (Spanwise domain: 4D) (d) Re=1000 (Spanwise domain: 4D) Fig.5 Isovorticity surface of instantaneous dynamic wake at Re=150,
More informationSimulation of Flow around a Surface-mounted Square-section Cylinder of Aspect Ratio Four
Simulation of Flow around a Surface-mounted Square-section Cylinder of Aspect Ratio Four You Qin Wang 1, Peter L. Jackson 2 and Jueyi Sui 2 1 High Performance Computing Laboratory, College of Science and
More informationChapter 5 Phenomena of laminar-turbulent boundary layer transition (including free shear layers)
Chapter 5 Phenomena of laminar-turbulent boundary layer transition (including free shear layers) T-S Leu May. 3, 2018 Chapter 5: Phenomena of laminar-turbulent boundary layer transition (including free
More informationPIV STUDY OF LONGITUDINAL VORTICES IN A TURBULENT BOUNDARY LAYER FLOW
ICAS CONGRESS PIV STUDY OF LONGITUDINAL VORTICES IN A TURBULENT BOUNDARY LAYER FLOW G. M. Di Cicca Department of Aerospace Engineering, Politecnico di Torino C.so Duca degli Abruzzi, 4 - I 19 Torino, ITALY
More informationExperimental and Numerical Investigation of Flow over a Cylinder at Reynolds Number 10 5
Journal of Modern Science and Technology Vol. 1. No. 1. May 2013 Issue. Pp.52-60 Experimental and Numerical Investigation of Flow over a Cylinder at Reynolds Number 10 5 Toukir Islam and S.M. Rakibul Hassan
More informationFlow control on a 3D backward facing ramp by pulsed jets
Acknowledgements: This work was carried out in the framework of the FOSCO project, supported by ic ARTS Flow control on a 3D backward facing ramp by pulsed jets 3 rd GDR Symposium P. Joseph a, D. Bortolus
More informationPractical application of active flow control is dependent upon the development of
Flow Control: the Renewal of Aerodynamics? D. Caruana, F. Rogier, G. Dufour, C. Gleyzes (Onera) E-mail: daniel.caruana@onera.fr The Plasma Synthetic Jet Actuator, Physics, Modeling and Flow Control Application
More informationRayleigh-Taylor Unstable Flames
Rayleigh-Taylor Unstable Flames Elizabeth P. Hicks 1,2 and Robert Rosner 2 CIERA, Northwestern University 1 University of Chicago 2 CIERA Conference: September 2, 2011 1 Type Ia Supernovae Image: NASA
More informationDetailed simulation of turbulent flow within a suction and oscillatory blowing fluidic actuator
Center for Turbulence Research Annual Research Briefs 14 9 Detailed simulation of turbulent flow within a suction and oscillatory blowing fluidic actuator By J. Kim AND P. Moin 1. Motivation and objectives
More informationDual Vortex Structure Shedding from Low Aspect Ratio, Surface-mounted Pyramids
Dual Vortex Structure Shedding from Low Aspect Ratio, Surface-mounted Pyramids Robert J. Martinuzzi Department of Mechanical and Manufacturing Engineering Schulich School of Engineering University of Calgary
More informationAerodynamic characteristics of two-dimensional sharp-edged objects in tandem arrangement )
Arch. Mech., 60, 6, pp. 475 490, Warszawa 2008 SIXTY YEARS OF THE ARCHIVES OF MECHANICS Aerodynamic characteristics of two-dimensional sharp-edged objects in tandem arrangement ) R. GNATOWSKA Institute
More informationInfluence of the Microplasma Actuator Electrode Configuration on the Induced EHD Flow
Proc. 2018 Electrostatics Joint Conference 1 Influence of the Microplasma Actuator Electrode Configuration on the Induced EHD Flow Marius Blajan, Daisuke Nonanka, Jaroslav Kristof and Kazuo Shimizu Organization
More informationPlasma Streamwise Vortex Generators for Flow Separation Control on Trucks
Flow Turbulence Combust (28) : 9 https://doi.org/.7/s494-8-989-9 Plasma Streamwise Vortex Generators for Flow Separation Control on Trucks A Proof-of-concept Experiment Julie A. Vernet,2 Ramis Örlü David
More informationUNIVERSITY OF CALGARY. Base Region Topology of Turbulent Wake around Finite Wall-Mounted Cylinder with. Application of Low Order Flow Representation
UNIVERSITY OF CALGARY Base Region Topology of Turbulent Wake around Finite Wall-Mounted Cylinder with Application of Low Order Flow Representation by Golriz Boorboor A THESIS SUBMITTED TO THE FACULTY OF
More informationTurbulent boundary layer
Turbulent boundary layer 0. Are they so different from laminar flows? 1. Three main effects of a solid wall 2. Statistical description: equations & results 3. Mean velocity field: classical asymptotic
More information2d-Laser Cantilever Anemometer
2d-Laser Cantilever Anemometer Introduction Measuring principle Calibration Design Comparative measurement Contact: Jaroslaw Puczylowski University of Oldenburg jaroslaw.puczylowski@forwind.de Introduction
More informationACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION
26th INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION F. Haucke, I. Peltzer, W. Nitsche Chair for Aerodynamics Department of Aeronautics
More informationNIHON. Experimental and Computational Study of Boundary Layer Transition by Two-Dimensional Roughness (January 1997) NIHON
ardekani@irost.ir NIHON Experimental and Computational Study of Boundary Layer Transition by Two-Dimensional Roughness (January 1997) NIHON The Mechanism of Boundary Layer Transition by Two-Dimensional
More information4' DTIC. ,.94 jl _ AD-A I ELEC -, ANNUAL REPORT 1 OCT 92 THROUGH 30 SEPT 93 C OFFICE OF NAVAL RESEARCH OCEAN TECHNOLOGY PROGRAM
AD-A274 845 ANNUAL REPORT DTIC I ELEC -, 0T 1 OCT 92 THROUGH 30 SEPT 93 C OFFICE OF NAVAL RESEARCH OCEAN TECHNOLOGY PROGRAM GRANT NUMBER: N00014-90J.4083 THE EFFECTS OF THREE-DIMENSIONAL IMPOSED DISTURBANCES
More informationSelf-Excited Vibration
Wenjing Ding Self-Excited Vibration Theory, Paradigms, and Research Methods With 228 figures Ö Springer Contents Chapter 1 Introduction 1 1.1 Main Features of Self-Excited Vibration 1 1.1.1 Natural Vibration
More informationMachine Learning: A change of paradigm in Flow Control?
Machine Learning: A change of paradigm in Flow Control? Laurent CORDIER Laurent.Cordier@univ-poitiers.fr PPRIME Institute Poitiers, France GDR CDD, Nantes, November 19, 2015 p.1/29 Flow control State of
More informationResponse of base suction and vortex shedding from rectangular prisms to transverse forcing
J. Fluid Mech. (2002), vol. 461, pp. 25 49. c 2002 Cambridge University Press DOI: 10.1017/S0022112002008534 Printed in the United Kingdom 25 Response of base suction and vortex shedding from rectangular
More informationOn the aeroacoustic tonal noise generation mechanism of a sharp-edged. plate
On the aeroacoustic tonal noise generation mechanism of a sharp-edged plate Danielle J. Moreau, Laura A. Brooks and Con J. Doolan School of Mechanical Engineering, The University of Adelaide, South Australia,
More informationReview on Vortex-Induced Vibration for Wave Propagation Class
Review on Vortex-Induced Vibration for Wave Propagation Class By Zhibiao Rao What s Vortex-Induced Vibration? In fluid dynamics, vortex-induced vibrations (VIV) are motions induced on bodies interacting
More informationFlow Characteristics around an Inclined Circular Cylinder with Fin
Lisbon, Portugal, 7- July, 28 Flow Characteristics around an Inclined Circular Cylinder with Fin Tsuneaki ISHIMA, Takeshi SASAKI 2, Yoshitsugu GOKAN 3 Yasushi TAKAHASHI 4, Tomio OBOKATA 5 : Department
More informationActive Control of Separated Cascade Flow
Chapter 5 Active Control of Separated Cascade Flow In this chapter, the possibility of active control using a synthetic jet applied to an unconventional axial stator-rotor arrangement is investigated.
More informationTransition of laminar pre-mixed flames to turbulence - induced by sub-breakdown applied voltage
Transition of laminar pre-mixed flames to turbulence - induced by sub-breakdown applied voltage Biswa N. Ganguly Aerospace Systems Directorate, Air Force Research Laboratory WPAFB OH USA and Jacob Schmidt
More informationDevelopment of a probe traversing system for an open test section wind tunnel
Development of a probe traversing system for an open test section wind tunnel Gépészet 2012 Conference 24 th of May, 2012 Section Energy 2. Árpád Varga Mechanical Engineering Modelling MSc, Contractual
More information