Transient energy growth for the Lamb???Oseen vortex, Physics of Fluids, vol.16, issue.1, 2004. ,
DOI : 10.1063/1.1626123
On vortex rings around vortices: an optimal mechanism, Journal of Fluid Mechanics, vol.578, pp.295-304, 2007. ,
DOI : 10.1017/S0022112007005198
Anomalous Self-Similarity in a Turbulent Rapidly Rotating Fluid, Physical Review Letters, vol.88, issue.11, p.88, 2002. ,
DOI : 10.1103/PhysRevLett.88.114501
Synthesis of ONERA chimera method developed in the frame of CHANCE program, 2005. ,
Meander of a fin trailing vortex and the origin of its turbulence, Experiments in Fluids, vol.387, issue.2, pp.599-611, 2010. ,
DOI : 10.1007/s00348-010-0825-0
On the relationship between blade circulation and tip vortex characteristics. 54th Annual Forum of the, pp.557-575, 1998. ,
Aerodynamic broadband noise from contra-rotating open rotors, 2011. ,
Broadband Noise Due to Rotor-Wake/Rotor Interaction in Contra-Rotating Open Rotors, AIAA Journal, vol.48, issue.11, pp.2674-2686, 2010. ,
DOI : 10.2514/1.J050566
Prediction of tip vortex self-induced parameters in terms of rotor blade loading, Proceedings of the American Helicopter Society Technical Specialists' Meeting on Aerodynamics and Aeroacoustics, 1987. ,
Assessment of aerodynamics and aeroacoustics tools for open rotors, European Turbomachinery Conference, 2011. ,
HPC Capabilities of The elsA CFD Software Applied to A Counter Rotating Open Rotor Test Rig, 30th AIAA Applied Aerodynamics Conference, pp.25-28, 2012. ,
DOI : 10.2514/6.2012-2777
Définition aérodynamique de l'hélice contrarotative HTC5. Etude et réalisation d'une balance de paroi pour essais d'hélices dans la soufflerie S3Ch, 1991. ,
Théorie de l'´ ecoulement tourbillonnant. Mémoires présentées par divers savantsà savantsà l'Académie des sciences de, pp.46-50, 1877. ,
Stabilité des paires de tourbillons contra-rotatifs : application au tourbillon de jeu dans les turbomachines, 2009. ,
Status of the elsA CFD software for flow simulation and multidisciplinary applications, 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008. ,
Modélisation analytique du bruit de raies des hélices contrarotatives . 10e Congrès Français d'Acoustique, pp.12-16, 2010. ,
Fast and accurate PIV computation using highly parallel iterative correlation maximization, Experiments in Fluids, vol.3, issue.2, pp.1169-1182, 2011. ,
DOI : 10.1007/s00348-011-1054-x
Turbulence en mécanique des fluides Analyse du phénomène en vue de sa modélisationmodélisation`modélisationà l'usage de l'ingénieur, 2000. ,
A general classification of three???dimensional flow fields, Physics of Fluids A: Fluid Dynamics, vol.2, issue.5, pp.765-777, 1990. ,
DOI : 10.1063/1.857730
Computational strategy for predicting CROR noise at low-speed Part II: investigation of the noise sources computation with the chorochronic method, 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), 2012. ,
DOI : 10.2514/6.2012-2222
Computational strategy for predicting CROR noise at low-speed Part I: review of the numerical methods, 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), 2012. ,
DOI : 10.2514/6.2012-2221
Computational strategy for predicting CROR noise at low-speed Part III: investigation of noise radiation with the Ffowcs-Williams Hawkings analogy, 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), 2012. ,
DOI : 10.2514/6.2012-2223
Helicopter tail rotor orthogonal balde vortex interaction, Progress in Aerospace Sciences, pp.453-489, 2004. ,
DOI : 10.1016/j.paerosci.2004.11.001
On the effectiveness and limitations of local criteria for the identification of a vortex, European Journal of Mechanics - B/Fluids, vol.18, issue.2, pp.261-282, 1999. ,
DOI : 10.1016/S0997-7546(99)80026-0
Aerodynamic and acoustic impact of a single protuberance placed on the leading edge of the front blades of an open rotor, 3AF 48th International Symposium of Applied Aerodynamic, 2013. ,
HeCToR-WP1 : Recensement de concepts de réduction du tourbillon marginal, Confidentiel Onera-Snecma, issue.2, 2010. ,
Cross-comparison of aerodynamic and acoustic predictions for open rotors with Onera (elsA-KIM) and DLR (TRACE-APSIM) codes. Onera-DLR Aerospace Symposium, 2011. ,
The structure and development of a wing-tip vortex, Journal of Fluid Mechanics, vol.14, issue.-1, pp.67-106, 1996. ,
DOI : 10.1088/0022-3735/18/5/012
Turbine and compressor employing tubercle leading edge rotor design. International Patent Number, assigned to WhalePower Corporation . International Filing Date, pp.27-31, 2006. ,
Some design philosophy for reducing the community noise of advanced couterrotation propellers, 1985. ,
Reduction of the noise of a model counterrotation propeller at cruise by reducing the aft propeller diameter, The Journal of the Acoustical Society of America, vol.81, issue.S1, 1987. ,
DOI : 10.1121/1.2024493
Vortex wakes of conventional aircraft, 1975. ,
Optimal Shape Design for Open Rotor Blades, 30th AIAA Applied Aerodynamics Conference, pp.2012-3018, 2012. ,
DOI : 10.2514/6.2012-3018
Short-wave cooperative instabilities in representative aircraft vortices, Physics of Fluids, vol.16, issue.5, pp.1366-1378, 2004. ,
DOI : 10.1063/1.1686951
Sound generation by turbulence and surfaces in arbitrary motion, Philosophical transactions of the Royal Society, vol.264, pp.321-342, 1969. ,
Flow past a delta wing with a sinusoidal leading edge: near-surface topology and flow structure, Experiments in Fluids, vol.42, issue.2, pp.321-331, 2009. ,
DOI : 10.1007/s00348-009-0666-x
Combining PIV, POD and vortex identification algorithms for the study of unsteady turbulent swirling flows, Measurement Science and Technology, vol.12, issue.9 ,
DOI : 10.1088/0957-0233/12/9/307
Optimising wing lift distribution to minimise wake vortex hasard. The Aeronautical Journal, pp.413-426, 2002. ,
Trailing Vortices from a Wing with a Notched Lift Distribution, AIAA Journal, vol.41, issue.9, pp.1835-1838, 2003. ,
DOI : 10.2514/2.7305
Fluid vortices, 1995. ,
Internal flow : Concepts and Applications, 2007. ,
DOI : 10.1017/CBO9780511616709
Initial assessment of open rotor propulsion applied to an advances single-aisle aircraft, Integration and Operations, 2001. ,
Advanced turboprop project. NASA SP-495, 1988. ,
The importance of quadrupole sources in prediction of transonic tip speed propeller noise, Journal of Sound and Vibration, vol.62, issue.1, pp.19-38, 1979. ,
DOI : 10.1016/0022-460X(79)90554-6
Shell model for rotating turbulence, Physical Review E, vol.70, issue.4, p.46311, 2004. ,
DOI : 10.1103/PhysRevE.70.046311
Wandering of wing-tip vortices, Proceedings of the 12th international symposium on applications of laser techniques to fluid mechanics, pp.35-38, 2004. ,
On the vortex formation over a slender wing at large angles of incidence. AGARD CP-247, 1979. ,
Eddies, stream and convergence zones in turbulent flows, pp.193-208, 1988. ,
ERATO : an ONERA-DLR cooperative programme on aeroacoustic rotor optimisation, 25th European Rotorcraft Forum, pp.14-16, 1999. ,
Aircraft wake vortices. Encyclopedia of Aerospace Engineering, 2010. ,
DOI : 10.1002/9780470686652.eae024
The properties of a transport aircraft wake in the extended near field - An experimental study, 39th Aerospace Sciences Meeting and Exhibit, 1038. ,
DOI : 10.2514/6.2001-1038
Homogeneous turbulence in the presence of rotation, Journal of Fluid Mechanics, vol.302, issue.-1, pp.1-52, 1990. ,
DOI : 10.1017/S0022112087003100
On the persistence of trailing vortices, Journal of Fluid Mechanics, vol.471, pp.159-168, 2002. ,
DOI : 10.1017/S0022112002002161
Time dependant calculations using multigrid, with applications to unsteady flows past airfoils and wings, pp.91-1596, 1991. ,
Acoustic characteristics of counterrotating unducted fans from model scale tests, Journal of aircraft, vol.27, issue.3, 1990. ,
On the identification of a vortex, Journal of Fluid Mechanics, vol.150, issue.-1, pp.69-94, 1995. ,
DOI : 10.1063/1.858826
Effects of Leading-Edge Protuberances on Airfoil Performance, AIAA Journal, vol.45, issue.11, p.45, 2007. ,
DOI : 10.2514/1.28497
Three-dimensional flows around low-aspect-ratio flat-plate wings at low reynolds numbers, Journal of Fluid Mechanics, vol.623, pp.187-207, 2009. ,
Effect of centerbody scattering on advanced openrotor noise, AIAA Journal, vol.48, issue.5, 2010. ,
Counter-Rotation Propeller Tip Vortex Interaction Noise, 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), 2009. ,
DOI : 10.2514/6.2009-3135
Resolving the Dependence on Freestream Values for the k- Turbulence Model, AIAA Journal, vol.38, issue.7, pp.1292-1295, 2000. ,
DOI : 10.2514/2.1101
On the formation and decay of rotor blade tip vortices. AIAA Paper 2004-2431 Fluid Mechanics Meeting, 2004. ,
Flowfield of a swept blade tip at high pitch angles, 29th Aerospace Sciences Meeting, 1991. ,
DOI : 10.2514/6.1991-704
Three-dimensional blade???vortex interaction in the strong vortex regime, Physics of Fluids, vol.10, issue.11, pp.2828-2845, 1998. ,
DOI : 10.1063/1.869805
Dense optical flow estimation by iterative local window registration, Proceedings of IEEE ICIP'05, pp.137-177, 2005. ,
Theoretical predictions for the elliptical instability in a twovortex flow, Journal of Fluid Mechanics, vol.471, pp.169-201, 2002. ,
URL : https://hal.archives-ouvertes.fr/hal-01430605
Mesure des déformations des maquettes : Mode d'emploi de OD2M, 2008. ,
FOLKI-PIV : une nouvelle apporche ultra-rapide pour le calcul de champs PIV stéréo, Congrès francophone de Techniques Laser septembre, Vandoeuvre-l` es-Nancy, pp.14-17, 2010. ,
A propos de l'instabilité des algorithmes de PIV itératifs, 20ème Congrés français de Mécanique, pp.29-31, 2011. ,
Aero-mechanical optimization of a contra-rotating open rotor and assessment of its aerodynamic and acoustic characteristics, European Turbomachinery Conference, 2011. ,
DOI : 10.1177/0957650911413695
Reynolds number, compressibility, and leading-edge bluntness effects on deltawing aerodynamics, 2004. ,
Propeller and propfan noise Aeroacoustics of Flight Vehicles : Theory and Practice, Noise sources, pp.1-64, 1991. ,
Vortex cutting by a blade. II - Computations of vortex response, AIAA Journal, vol.32, issue.7, pp.1428-1436, 1994. ,
DOI : 10.2514/3.12212
Influence of periodic unsteady effects on flow and performance prediction on an axial high pressure compressor ,
URL : https://hal.archives-ouvertes.fr/hal-01011305
Two-equation eddy-viscosity turbulence models for engineering applications, AIAA Journal, vol.32, issue.8, pp.1598-1605, 1994. ,
DOI : 10.2514/3.12149
Benefits of blade sweep for advanced turboprops, Journal of Propulsion and Power, vol.2, issue.6, pp.534-540, 1986. ,
DOI : 10.2514/3.22938
Experimental Evaluation of Sinusoidal Leading Edges, Journal of Aircraft, vol.44, issue.4, 2007. ,
DOI : 10.2514/1.30303
) flippers, Physics of Fluids, vol.16, issue.5, 2004. ,
DOI : 10.1063/1.1688341
Summary and recent results from the NASA advanced high-speed propeller research program, 18th Joint Propulsion Conference, 1982. ,
DOI : 10.2514/6.1982-1119
Linear and nonlinear interactions between a columnar vortex and external turbulence, Journal of Fluid Mechanics, vol.402, pp.349-378, 2000. ,
DOI : 10.1017/S0022112099006990
Decaying grid-turbulence in a rotating tank, Physics of fluids, vol.17, 2005. ,
Control of vortical structures on a flapping wing via a sinusoidal leading-edge, Physics of Fluids, vol.22, issue.2, p.21701, 2010. ,
DOI : 10.1063/1.3304539
Theoretical prediction of counter-rotating propeller noise ,
Relative importance of open rotor tone and broadband noise sources, 17th AIAA/CEAS Aeroacoustics Conference, pp.5-8 ,
Aeroacoustic tests of isolated open rotors at high speed, 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), 2012. ,
DOI : 10.2514/6.2012-2220
A Project Study of Open Rotor Noise, International Journal of Aeroacoustics, vol.449, issue.12, 2012. ,
DOI : 10.1260/1475-472X.11.2.247
Numerical study of stall delay on humpback whale flippers, 46th AIAA Aerospace Sciences Meeting and Exhibit, pp.7-10, 2008. ,
Rotor interaction noise in counter-rotating propfan propulsion systems, Journal of Turbomachinery, vol.134, issue.1, 2012. ,
A concept of the vortex lift of sharp-edged delta wings based on a leading-edge suction analogy ,
Turbulent Flows, 2000. ,
URL : https://hal.archives-ouvertes.fr/hal-00338511
Transient growth of perturbations in a vortex column, Journal of Fluid Mechanics, vol.550, issue.-1, pp.251-288, 2006. ,
DOI : 10.1017/S0022112005008207
Comparison of Ffowcs Williams-Hawkings and Kirchhoff rotor noise calculations, 4th AIAA/CEAS Aeroacoustics Conference, pp.98-2376, 1998. ,
DOI : 10.2514/6.1998-2376
On the Motion of Solids in a Liquid Possessing Vorticity, Proceedings of the royal society A, 92, p.408, 1916. ,
DOI : 10.1098/rspa.1916.0026
Particle Image Velocimetry, 2007. ,
DOI : 10.1007/978-3-662-03637-2
Manuel utilisateur du logiciel acoustique KIM -Version 6.2. DSNA, Février, 2009. ,
On the dynamics of revolving fluids, Proceedings of the royal society A, pp.148-154, 1917. ,
Simulation et modélisation de la transition par bulbe de décollement laminaire Application au décrochage dynamique, 2008. ,
Installation Effects on Contra-Rotating Open Rotor Noise, 16th AIAA/CEAS Aeroacoustics Conference, 2010. ,
DOI : 10.2514/6.2010-3795
On open rotor blade-vortex interaction noise, 2012. ,
On the Inviscid Rolled-Up Structure of Lift-Generated Vortices, Journal of Aircraft, vol.10, issue.11, 1973. ,
DOI : 10.2514/3.60277
Prediction of Span Loading from Measured Wake-Vortex Structure -An Inverse Betz Method, Journal of Aircraft, vol.12, issue.7, pp.626-628, 1975. ,
DOI : 10.2514/3.59845
Prediction of Viscous Trailing Vortex Structure from Basic Loading Parameters, AIAA Journal, vol.36, issue.2, pp.208-218, 1988. ,
DOI : 10.2514/2.7503
Rotor-vortex interaction noise, 8th Aeroacoustics Conference, 1983. ,
DOI : 10.2514/6.1983-720
Aerodynamic and basic acoustic optimization of a contra-rotating open rotor with experimental verification, 18th AIAA/CEAS Aeroacoustics Conference, 2012. ,
Transfert of energy to two-dimensional large scales in forced, rotating three-dimensional turbulence, Physics of fluids, vol.11, 1999. ,
Analytical Methods for the Development of Reynolds-Stress Closures in Turbulence, Annual Review of Fluid Mechanics, vol.23, issue.1, 1991. ,
DOI : 10.1146/annurev.fl.23.010191.000543
Technology and benefits of aircraft counter rotation propellers, 1982. ,
Aerodynamic and aeroacoustic installation effects for pusherconfiguration CROR propulsion systems, 28th Applied Aerodynamics Conference, 2010. ,
Note on the connection between the lift on an airfoil in a wind tunnel and the circulation round it, Philosophical Transactions of the Royal Society, Series A, vol.225, pp.238-245, 1925. ,
Pale pour une hélice de turbomachinè a soufflante non carénée, hélice et turbomachine correspondantes, 2011. ,
The aerodynamics of propellers, Progress in Aerospace Science, pp.85-128, 2006. ,
DOI : 10.1016/j.paerosci.2006.04.001
On the influence of trailing-edge serrations on openrotor tonal noise, 18th AIAA/CEAS Aeroacoustics Conference, pp.4-06, 2012. ,
A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets, 1976. ,
Noise of a model counterrotation propeller with reduced aft rotor diameter at simulated takeoff/approach conditions (F7/A3) AIAA 26th Aerospace Sciences Meeting, 1988. ,
Numerical study of rotating turbulence with exernal forcing, 1998. ,
Effect of the wavy leading edge on hydrodynamic characteristics for flow around low aspect ratio wing, Computers & Fluids, vol.49, issue.1, pp.276-289, 2011. ,
DOI : 10.1016/j.compfluid.2011.06.010
Contra-rotating open rotor operation for improved aerodynamics and noise at take-off, Proceedings of ASME Turbo Expo, pp.2011-45205, 2011. ,
The persistence of trailing vortices: A modeling study, Physics of Fluids, vol.7, issue.1, p.135, 1995. ,
DOI : 10.1063/1.868734
Multigrid Computation of Incompressible Flows Using Two-Equation Turbulence Models: Part I???Numerical Method, Journal of Fluids Engineering, vol.119, issue.4, pp.893-905, 1997. ,
DOI : 10.1115/1.2819513
A phenomenological treatment of rotating turbulence, Physics of Fluids, vol.7, issue.8, pp.2092-2094, 1995. ,
DOI : 10.1063/1.868457