Program

	Monday (23rd March)	Tuesday (24th March)	Wednesday (25th March)	Thursday (26th March)
Session 1 (morning): 8:30 – 10:30	Welcome Invited talk: Eric Moreau Plasma flow Control A (3)	Invited talk: Jinjun Wang Synthetic jets (3) Jet flows A (1)	Invited talk: Preetinder Virk Polymers (1) Laser Energy Deposition (1) Hydrophobic surfaces A (2)	Invited talk: Alfredo Pinelli Compliant structures (4)
	Coffee break: 30 min
Session 2 (morning): 11:00 – 13:00	Plasma flow Control B (4) Icing control (2)	Jet flows B (3) Noise control (2)	Hydrophobic surfaces B (4) Wall oscillations A (2)	Laminar flow control (6)
	Lunch break: 1 hour 20 min
Session 3 (afternoon): 14:20– 16:00	Riblets (5)	Excursion	Wall oscillations B (4) Turbulent flow control A (1)	Flow separation control (4)
	Coffee break: 30 min		Coffee break: 30 min
Session 4 (afternoon): 16:30 – 17:50	Roughness (4)		Turbulent flow control B (4)	Round table
	Dinner (18:45)		Banquet (19:30)

List of papers

(pdf version)

Plasma flow control

• FLOW CONTROL BY PLASMA ACTUATORS (Invited lecture)

E. Moreau, N. Benard

CNRS, University of Poitiers

• NUMERICAL STUDY OF REDUCING TURBULENT SKIN-FRICTION DRAG USING DBD PLASMA ACTUATORS

Qiang Yang, Yongmann M. Chung

University of Warwick

• NUMERICAL MODELLING OF CROSS-FLOW DOMINATED TRANSITION CONTROL BY MULTIPLE-ELECTRODES DBD ACTUATORS

D.A. Russianov, M. V. Ustinov

TSAGI

• CAUSE-EFFECT RELATIONS BETWEEN DISCHARGE CAPACITANCE AND VOLUME FORCES OF DBD PLASMA ACTUATORS

M. Kuhnhenn, B. Simon, I. Maden, S. Grundmann

TU Darmstadt

J. Kriegseis

KIT

• CONTROL MECHANISM OF DBD PLASMA ACTUATOR FOR DEEP-STALL FLOW AROUND NACA0015 AT RE= 6.3X10^4

H. Kato

University of Tokyo

M. Sato, H. Aono, A. Yakeno, K. Fujii

JAXA

• FLAT PLATE VORTEX SHEDDING NOISE SUPPRESSION WITH SURFACE DIELECTRIC BARRIER DISCHARGE PLASMA ACTUATORS

A. Laith, T. P. Chong

Brunel University London

J. H. Kim

University of Nottingham

• CONTROL OF THE LEADING-EDGE FLOW SEPARATION USING DBD PLASMA ACTUATORS

Longfei Song and Kwing-SoChoi

University of Nottingham

• DISTRIBUTED FORCING OF THE WAKE OF A BLUNT TRAILING EDGE PROFILED BODY USING PLASMA ACTUATORS TO REDUCE PRESSURE DRAG

A.Naghib-Lahouti,P. Lavoie

University of Toronto Institute for Aerospace Studies

Icing control

• ANN MODEL FOR ICE SHAPE PREDICTION OF AN AIRFOIL

Zhen Tian

Shanghai Jiao Tong University

Kwing-SoChoi

University of Nottingham

• THE ACCRETION OF MIXED ICE ON AN AIRCRAFT WING DUE TO THE PARTIAL FREEZING OF IMPINGING SUPERCOOLED DROPLETS

Janjua, Z.A., Turnbull, B., Hibberd, S., Choi,K-S.

University of Nottingham

Riblets

• RIBLET DRAG REDUCTION AND THE EFFECT OF BULK FLUID ROTATION IN A FULLY TURBULENT TAYLOR-COUETTE FLOW

A.J. Greidanus, R. Delfos, S. Tokg�z, J. Westerweel

Delft University of Technology

• EXPERIMENTAL AND NUMERICAL INVESTIGATION OF RIBLETS IN A FULLY DEVELOPED TURBULENT CHANNEL FLOW

V. Fink, A. G�ttler, B. Frohnapfel

KIT

• EFFECT OF RIBLETS ON A COMPLEX CONFIGURATION IN TRANSONIC CONDITIONS

B. Mele, R. Tognaccini

University Federico II Napoli

P. Catalano

CIRA

• THERMAL RIBLETS: CONCEPTUAL APPROACH TO FLOW CONTROL

N. Yurchenko

Institute of Hydromechanics NASU

• LINEARLY OPTIMAL SPANWISE BOUNDARY MODULATIONS FOR WAKE INSTABILITY CONTROL

O. Tammisola

University of Nottingham

Surface roughness

• TURBULENT DRAG REDUCTION BY POROUS COATINGS

N. Abderrahaman, R.Garcia-Mayoral

University of Cambridge

• REGULAR AND IRREGULAR SURFACES IN TURBULENT CHANNEL FLOWS

D. Sassun, P. Orlandi

Universit� di Roma La Sapienza

• TURBULENT DRAG REDUCTION DUE TO ELECTROSTATIC FLOCKING SURFACE WITH GROOVES

S. Tamano, H. Kurisaki, H. Ikarashi, and Y. Morinishi

Nagoya Institute of Technology

Synthetic jets

• ACTIVE FLOW CONTROL USING SYNTHETIC JETS (Invited lecture)

J. J. Wang, L. H. Feng

Beijing University of Aeronautics and Astronautics

• CONTROL OF NEAR-WALL STRUCTURES IN A TURBULENT BOUNDARY LAYER USING SYNTHETIC JETS

E. Spinosa, S. Zhang, S. Zhong

University of Manchester

• SPATIO-TEMPORAL COHERENT FLOW STRUCTURE EVOLUTION OF ZNMF JET CONTROLLED NACA 0015 AIRFOIL FLOW

J. Soria, C. Atkinson, N. Buchman, V. Kitsios

Monash University Melbourne

• NUMERICAL OPTIMIZATION OF AZERO-NET-MASS-FLUX ACTUATION FOR A HIGH LIFT AIRFOIL

V. Ciobaca

DLR

Jet flows

• FLOW CONTROL USING ANNULAR JETS

T. Jukes, J. Lirvat, F. Nicolas

Dyson

G. R. Hunt

University of Cambridge

• SYSTEMS ARCHITECTURE AND IMPLEMENTATION COSTS OF SWEEPING JET ACTUATORS FOR SEPARATION CONTROL

M. Jabbal

Brunel University

S. Raghu

Advanced Fluidics LLC, USA

• CONTROL OF CAVITY-INDUCED DRAG USING STEADY JETS

N. Al Haddabi, K. Kontis, H.Zare-Behtash,S.Winblad-Rasmussen

University of Glasgow

• CONTROL OF WING LOADS BY MEANS OF BLOWING AND MINI-TABS

D.J. Heathcote, N.Al-Battal,I. Gursul, D.J. Cleaver

University of Bath

Noise control

• LARGE EDDY SIMULATION OF A FLOW CONTROL DEVICE FOR NOISE REDUCTION DUE TO A CROR/PYLON INTERACTION

N. Gourdain, Y. Bury, L. Dupont, J. Bodart and L. Joly

ISAE, Toulouse

• CONTROL OF CAVITY TONE BY SPANWISE ALIGNED JETS IN UPSTREAM BOUNDARY LAYER

H. Yokoyama, R. Adachi, T. Minato, H. Odawara, H. Morishima and A. Iida

Toyohashi University of Technology

Polymers

• FLOW DEVELOPMENT AND DEGRADATION IN THE POLYMERIC AND MAXIMUM DRAG REDUCTION REGIMES (invited lecture)

P. S. Virk, A. L. Shields

Massachusetts Institute of Technology

• A NOVEL DRAG-REDUCING COATING MATERIAL: FDR-SPC (FRICTIONAL DRAG REDUCTION SELF-POLISHING COPOLYMER)

Inwon Lee, Hyun Park, Ho Hwan Chun

Pusan National University

Laser Energy Deposition

• DRAG FORCE CONTROL FOR HEMISPHERE-CYLINDER UNDER THE ACTION OF LASER ENERGY DEPOSITION

O. A. Azarova

Dorodnicyn Computing Center of RAS Moscow

D. D. Knight

Rutgers University, New Jersey

Hydrophobic surfaces

• A MODEL FOR TURBULENT DRAG REDUCTION OVER LIQUID INFUSED MICRO-TEXTURED SURFACES

M. K. Fu, M. Hultmark

Princeton University

• INFLUENCE OF SURFACE PATTERN ON SLIP LENGTHS FOR SUPERHYDROPHOBIC SURFACES

C. T. Fairhall, R.Garcia-Mayoral

University of Cambridge

• DYNAMIC RESPONSE OF GAS-LIQUID INTERFACES IN SUPERHYDROPHOBIC SURFACES

R.Garcia-Mayoral

University of Cambridge

J. Seo, A. Mani

Stanford University

• REDUCTION OF TURBULENT FRICTION BY HYDROPHOBIC SURFACES WITH SHEAR-DEPENDENT SLIP LENGTHS

S. Khosh Aghdam, P. Ricco, M. Seddighi

University of Sheffield

• THE RELEVANCE OF LONGITUDINAL AND TRANSVERSE PROTRUSION HEIGHTS FOR DRAG REDUCTION BY A SUPERHYDROPHOBIC SURFACE

P. Luchini

Universita di Salerno

• TRANSITION DELAY IN PLANE CHANNEL FLOW USING SUPERHYDROPHOBIC COATING

J. O. Pralits and A. Bottaro

Universita di Genova

Wall oscillation and rotation

• DRAG-REDUCING WALL OSCILLATIONS VIA DIELECTRIC ELASTOMER ACTUATORS IN LOW REYNOLDS NUMBER INTERNAL TURBULENT FLOWS

D. Gatti, A. G�ttler, B. Frohnapfel, C. Tropea

KIT

• SKIN-FRICTION DRAG REDUCTION BY SPANWISE FORCING: THE REYNOLDS-NUMBER EFFECT

M. Quadrio Politecnico di Milano D. Gatti

KIT

• COMBINATION OF WALL TRANSPIRATION AND SPINNING RINGS FOR TURBULENT DRAG REDUCTION

P. Ricco, S. Khosh Aghdam, M. Seddighi

University of Sheffield

• OSCILLATING DISCS FOR TURBULENT DRAG REDUCTION

D.J. Wise, P. Ricco

University of Sheffield

• TURBULENT DRAG REDUCTION VIA SPINNING DISCS AND RINGS.

C. Alvarenga, D.J. Wise, P. Ricco

University of Sheffield

• IN-PLANE FORCING OF A TURBULENT BOUNDARY LAYER, THROUGH THE ACTUATION OF A COMPLIANT STRUCTURE.

J. Bird, M. Santer, J. F. Morrison

Imperial College London

Turbulent flow control

• ON THE RELATION BETWEEN NEAR-WALL SKIN FRICTION AND LARGE-SCALE COHERENT MOTIONS IN TURBULENT BOUNDARY LAYERS

A. Basso, N. Rkiouak,K.-S.Choi

University of Nottingham

• SKIN FRICTION DRAG REDUCTION USING UNSTEADY BLOWING THROUGH ONE ARRAY OF STREAMWISE SLITS

Yinzhe Li, Yu Zhou

Harbin Institute of Technology, Shenzhen, China

• DOWNSTREAM DEVELOPMENT OF LOCALLY CONTROLLED TURBULENT BOUNDARY LAYER

A. Stroh, B. Frohnapfel

KIT

P. Schlatter

KTH

Y. Hasegawa

University of Tokyo

• ON WHY CONTROL OF TURBULENT FLOWS IS NON-TRIVIAL AND WHY IT IS POSSIBLE

A. Tsinober

Tel Aviv University

Compliant surfaces and structures

• INTERACTION OF FLEXIBLE FILAMENTS WITH THE WAKE OF CYLINDER AT LOW REYNOLDS NUMBERS (Invited lecture)

M. Omidyeganeh and A. Pinelli

City University London

• STUDY OF FLOW AROUND NACA0020 AEROFOIL WITH HAIRY FLAPS DURING RAMP-UP MOTION

M. E. Rosti, M. Omidyeganeh and A. Pinelli

City University London

• DRAG REDUCTION OF A SQUARE CYLINDER USING COMPLIANT FLAPS

N. Mazellier, A. Feuvrier, A. Kourta

Univ. Orl�ans

• CONTROL FOR FLAT PLATE SKIN-FRICTION DRAG WITH COMPLIANT COATINGS (PREDICTIONS AND EXPERIMENT)

V. M. Kulik, A.V. Boiko

Russian Academy of Sciences, Novosibirsk

Ho Hwan Chun, Inwon Lee

Pusan National University

• WAVE PROPERTIES OF A COMPLIANT COATING IN A FLUID FLOW

V. Vedeneev

Lomonosov Moscow State University

Laminar and transition control

• RECENT INVESTIGATIONS INTO LAMINAR FLOW CONTROL FOR NACELLE APPLICATION

James Tweedie, Liam Magee

Bombardier Aerospace Belfast, UK

• SIMULATION OF PRESSURE LOSSES FOR THE DESIGN OF TAILORED SUCTION DISTRIBUTIONS FOR LAMINAR FLOW CONTROL

P. Scholz, L. Klug

TU Braunschweig

L.M.M. Boermans

TU Delft

• ADAPTIVE SECONDARY PATH FOR ADAPTIVE CONTROLLERS IN LAMINAR BOUNDARY LAYER CONTROL

B. Simon, T. Nemitz, S. Grundmann, J. Rohlfing, F. Fischer

TU Darmstadt

D. Mayer

Fraunhofer Darmstadt

• EXPERIMENTS ON ACTIVE CONTROL OF TOLLMIEN-SCHLICHTING WAVES: CANCELLATION BY WAVE SUPERPOSITION AND SPACE-TIME TRANSFER FUNCTIONS FOR FEEDBACK LOOP

H. Vemuri, J.F. Morrison, E.C. Kerrigan

Imperial College London

• RELAMINARISATION OF TURBULENT CHANNEL FLOW WITH PASSIVITY-BASED LINEAR FEEDBACK CONTROL

K. Septham, J. F. Morrison

Imperial College London

• RECENT PROGRESS USING THE AFRODITE FLOW CONTROL STRATEGY

R. S. Downs and J. H. M. Fransson

KTH

Flow separation control

• DRAG REDUCTION ON A SIMPLIFIED 3D BLUFF BODY

C. Sardu, S. Sedda, G. Iuso

Politecnico di Torino

• EXPERIMENTAL OPEN-LOOP AND CLOSED-LOOP CONTROL OF A MASSIVE SEPARATED BOUNDARY LAYER AT HIGH REYNOLDS NUMBER

C. Raibaudo, A. Polyakov, J.P. Richard, F. Kerherv�, M. Stanislas

Ecole Centrale de Lille, CNRS

• FLOW OVER NACA0012 AIRFOIL INFLUENCED BY UPSTREAM CIRCULAR CYLINDER WAKE

Wu J., Feng L., Pan C., Gao Q., Li T., Wang J.

Beijing University of Aeronautics & Astronautics and AVIC Shenyang Aircraft Design and Research Institute, Shenyang