Superposition of the spanwise distribution of thrust dF x dr (in N/m) with the wall pressure distribution and friction lines for different blade geometries at iso-thrust, at take-off Bibliography Fundamentals of Aerodynamics, Figure 7.9, 2007. ,
Near- and far-field aerodynamics in insect hovering flight: an integrated computational study, Journal of Experimental Biology, vol.211, issue.2, pp.239-257, 2007. ,
DOI : 10.1242/jeb.008649
URL : http://jeb.biologists.org/content/jexbio/211/2/239.full.pdf
Smoothing Periodograms from Time-Series with Continuous Spectra, Nature, vol.161, issue.4096, pp.686-687, 1948. ,
DOI : 10.1038/161686a0
A low order method for co-axial propeller and rotor performance prediction, 29th Congrees of the International Council of the Aerautical Sciences, 2014. ,
URL : https://hal.archives-ouvertes.fr/hal-01079555
Some developments in the theory of vortex breakdown, Journal of Fluid Mechanics, vol.1, issue.01, pp.65-84, 1967. ,
DOI : 10.1115/1.3650590
3d numerical predictions of horizontal axis wind turbine power characteristics of the scaled delft university t40/50 model, Fifth JSME-KSME Fluids Engineering Conference, 2002. ,
Aerodynamics for Engineers, 2014. ,
Spanwise flow and the attachment of the leading-edge vortex on insect wings, Nature, vol.200, issue.6848, pp.412729-733, 2001. ,
DOI : 10.1103/PhysRevLett.85.2216
A Non-linear Wing Theory and its Application to Rectangular Wings of Small Aspect Ratio, Zeitschrift für Angewandte Mathematik und Mechanik, pp.21-35, 1939. ,
DOI : 10.1002/zamm.19390190103
Wind turbine tip-loss corrections: review, implementation and investigation of new models. Master's thesis, Risø-DTU, Siemens Energy Inc.(available at DTU's library), 2011. ,
Effect of Leading-Edge Separation on the Lift of a Delta Wing, Journal of the Aeronautical Sciences, vol.21, issue.10, pp.690-706, 1954. ,
DOI : 10.2514/8.2663
On slender delta wings with leading-edge separation, 1955. ,
A rotary wing system for micro air vehicle applications. part 1, Incas Bulletin, vol.3, issue.3, pp.23-33, 2011. ,
CFD software: input from research and feedback from industry, Mechanics & Industry, vol.123, issue.3, pp.159-174, 2013. ,
DOI : 10.1115/1.1369598
URL : https://hal.archives-ouvertes.fr/hal-01293795
Fast and accurate piv computation using highly parallel iterative correlation maximization, Experiments in Fluids, vol.50, issue.4, pp.1169-1182, 2011. ,
An introduction to the proper orthogonal decomposition, Current science, vol.78, issue.7, pp.808-817, 2000. ,
Influence of torque ratio on counter rotating open rotor interaction noise, 20th AIAA/CEAS Aeroacoustics Conference, 2014. ,
Influence of Torque Ratio on Counter-Rotating Open-Rotor Interaction Noise, AIAA Journal, vol.7, issue.14, pp.2726-2738, 2015. ,
DOI : 10.2514/6.2011-2758
Open rotor interaction noise reduction through front rotor wake modification, International Journal of Aeroacoustics, vol.74, issue.1-2, pp.207-227, 2016. ,
DOI : 10.1016/0376-0421(94)90002-7
Swept and curved wings: a numerical approach based on generalized lifting-line theory, Computational Mechanics, vol.29, issue.4-5, pp.4-5322, 2002. ,
DOI : 10.1007/s00466-002-0345-8
An experimental investigation of the structure of a leading-edge vortex, 1961. ,
Low-speed windtunnel experiments on a series of sharp-edged delta wings, 1964. ,
Evolution of the Leading-Edge Vortex over an Accelerating Rotating Wing, Procedia IUTAM, 2013. ,
DOI : 10.1016/j.piutam.2013.03.027
Leading-edge vortices in insect flight, Nature, vol.384, issue.6610, pp.626-630, 1996. ,
DOI : 10.1038/384626a0
Analysis of computed flow parameters for a set of sudden stalls in low-speed two-dimensional flow, National Aeronautics and Space Administration, 1959. ,
Lift and the leading-edge vortex, Journal of Fluid Mechanics, vol.57, pp.280-313, 2013. ,
DOI : 10.1017/jfm.2011.490
Turbulent and unsteady flow characteristics of delta wing vortex systems, Aerospace Science and Technology, vol.24, issue.1, pp.32-44, 2013. ,
DOI : 10.1016/j.ast.2012.08.007
Dynamics of revolving wings for various aspect ratios, Journal of Fluid Mechanics, vol.205, pp.932-956, 2014. ,
DOI : 10.1007/s00348-010-0872-6
Three-dimensional flow structure and aerodynamic loading on a revolving wing, Physics of fluids, vol.25, pp.932-956, 2013. ,
Calculation of non-linear aerodynamic stability derivatives of aeroplanes, 1961. ,
Unsteady vortex structure over a delta wing, Journal of Aircraft, vol.1259, issue.1, pp.243-248, 1994. ,
DOI : 10.2514/6.1990-102
Higher-order compact difference scheme applied to the simulation of a low sweep delta wing flow, 41 st AIAA Aerospace Sciences Meeting & Exhibit, 2003. ,
Compact Difference Scheme Applied to Simulation of Low-Sweep Delta Wing Flow., AIAA Journal, vol.1259, issue.8, pp.431744-1752, 2005. ,
DOI : 10.2514/2.1644
High-Order Simulation of Low Sweep Delta Wing Flows Using a Hybrid RANS/ILES Model, 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006. ,
DOI : 10.2514/6.2003-3889
Computational and experimental investigation of a nonslender delta wing, AIAA journal, issue.8, p.471811, 2009. ,
Combining PIV, POD and vortex identification algorithms for the study of unsteady turbulent swirling flows, Measurement Science and Technology, vol.12, issue.9, p.1422, 2001. ,
DOI : 10.1088/0957-0233/12/9/307
A generalized lifting-line theory for curved and swept wings, Journal of Fluid Mechanics, vol.307, issue.-1, pp.497-513, 1990. ,
DOI : 10.1007/BF01601487
A unified unsteady lifting-line theory, Journal of Fluid Mechanics, vol.32, issue.-1, pp.427-451, 1991. ,
DOI : 10.1017/S0022112057000440
Aerodynamics of wind turbines Routledge, 2000. ,
Noise of counter-rotation propellers, Journal of Aircraft, vol.123, issue.7, pp.609-617, 1985. ,
DOI : 10.1121/1.1914455
Reynolds number and aspect ratio effects on the leading-edge vortex for rotating insect wing planforms, Journal of Fluid Mechanics, vol.52, pp.166-192, 2013. ,
DOI : 10.1007/s10409-005-0072-4
Some observations of the vortex breakdown phenomenon, Journal of Fluid Mechanics, vol.14, issue.04, pp.585-592, 1962. ,
DOI : 10.1017/S0022112062001470
Connection between leading-edge sweep, vortex lift, and vortex strength for delta wings, Journal of Aircraft, vol.1987, issue.5, pp.473-475, 1989. ,
DOI : 10.1016/0021-8928(60)90033-2
Experimental lift of low aspect-ratio triangular wings at large angles of attack and supersonic speeds, Bibliography, 1957. ,
Aspects of the modelling and numerical simulation of leading-edge vortex flow, IUTAM Symposium on Fluid Dynamics of High Angle of Attack, 1992. ,
Laminar separation bubbles in two or three dimensional incompressible flow, 1968. ,
Aerodynamics for engineering students, 2003. ,
Wind turbine blade analysis using the blade element momentum method. version 1.0, 2005. ,
The properties of a transport aircraft wake in the extended near field - An experimental study, 39th Aerospace Sciences Meeting and Exhibit, 1038. ,
DOI : 10.1146/annurev.fl.07.010175.001041
Resolving the Dependence on Freestream Values for the k- Turbulence Model, AIAA Journal, vol.490, issue.16, pp.1292-1295, 2000. ,
DOI : 10.1063/1.868241
Leading-edge vortex shedding from rotating wings, Fluid Dynamics Research, vol.46, issue.3, p.31421, 2014. ,
DOI : 10.1088/0169-5983/46/3/031421
URL : https://hal.archives-ouvertes.fr/hal-01299245
Extension of the leading-edge suction analogy to wings with separated flow around the side edges at subsonic speeds, 1974. ,
Some recent applications of the suction analogy to vortexlift estimates, 1975. ,
The bursting of leadingedge vortices -some observations and discussion of the phenomenon, 1961. ,
Low-speed windtunnel measurements on a thin sharp-edged delta wing with 70 degrees leading-edge sweep, with particular reference to the position of leading-edge vortex breakdown, 1961. ,
Lift Force of Delta Wings, Applied Mechanics Reviews, vol.43, issue.9, pp.209-221, 1990. ,
DOI : 10.1115/1.3119169
Ecoulement au voisinage de la pointe avant d'une aile à forte flèche aux incidences moyennes, La recherche aéronautique, vol.30, pp.3-8, 1952. ,
Biofluiddynamic scaling of flapping, spinning and translating fins and wings, Journal of Experimental Biology, vol.212, issue.16, pp.2691-2704, 2009. ,
DOI : 10.1242/jeb.022251
Rotational accelerations stabilize leading edge vortices on revolving fly wings, Journal of Experimental Biology, vol.212, issue.16, pp.2705-2719, 2009. ,
DOI : 10.1242/jeb.022269
URL : http://jeb.biologists.org/content/jexbio/212/16/2705.full.pdf
Vortex-wake interactions of a flapping foil that models animal swimming and flight, The Journal of Experimental Biology, vol.211, pp.267-273, 2008. ,
Aero-mechanical optimization of a contra-rotating open rotor and assessment of its aerodynamic and acoustic characteristics, Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, pp.225850-863, 2011. ,
DOI : 10.2514/2.558
Experimental Investigation of the Turbulent Structure of Vortex Wakes, 4th Symposium on Turbulent Shear Flows, 1983. ,
DOI : 10.1007/978-3-642-69996-2_12
ON THE PROLONG ATTACHMENT OF LEADING EDGE VORTEX ON A FLAPPING WING, Modern Physics Letters B, vol.590, issue.03, pp.357-360, 2009. ,
DOI : 10.1143/JPSJ.71.1622
Modelling of rotational augmentation based on engineering considerations and measurements, European Wind Energy Conference, 2004. ,
Dual leading-edge vortices on flapping wings, Journal of Experimental Biology, vol.209, issue.24, pp.5005-5016, 2006. ,
DOI : 10.1242/jeb.02614
URL : http://jeb.biologists.org/content/jexbio/209/24/5005.full.pdf
The Development of the Slender Delta Concept, Aircraft Engineering and Aerospace Technology, vol.40, issue.3, pp.12-17, 1968. ,
DOI : 10.1108/eb034350
A heory of the flow past a slender delta wing with leading-edge separation, Proceedings of the Royal Society A, pp.200-217, 1959. ,
The Fluid Dynamics of Insect Flight, Annual Review of Fluid Mechanics, vol.13, issue.1, pp.329-350, 1981. ,
DOI : 10.1146/annurev.fl.13.010181.001553
The formation and maintenance of a leading-edge vortex during the forward motion of an animal wing, Journal of Fluid Mechanics, vol.352, pp.471-475, 2007. ,
DOI : 10.1038/384626a0
Unsteady nature of leading edge vortices, Physics of Fluids, vol.9, issue.10, pp.2960-2966, 1997. ,
DOI : 10.1146/annurev.fl.16.010184.002053
Two-equation eddy-viscosity turbulence models for engineering applications, AIAA Journal, vol.32, issue.8, pp.1598-1605, 1994. ,
DOI : 10.2514/6.1979-1479
Vortical substructures in the shear layers forming leading-edge vortices, AIAA journal, issue.8, pp.401689-1692, 2002. ,
The role of the leading edge vortex in lift augmentation of steadily revolving wings: a change in perspective, Journal of The Royal Society Interface, vol.50, issue.132, p.1420170159, 2017. ,
DOI : 10.2514/1.C032128
The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude manoeuvers, Progress in Aerospace Sciences, pp.185-248, 2003. ,
A simple solution method for the blade element momentum equations with guaranteed convergence, Wind Energy, vol.17, issue.9, pp.1327-1345, 2014. ,
Leading-edge vortex structure of nonslender delta wings at low reynolds number, AIAA journal, vol.41, issue.1, pp.16-132, 2003. ,
Flow structure on a rotating plate, Experiments in Fluids, vol.327, issue.4864, pp.207-223, 2012. ,
DOI : 10.1098/rstb.1990.0040
Contribution a l'etude experimentale et theorique de l'eclatement tourbillonnaire en air incompressible, 1989. ,
Surface Pressure Estimates for Pitching Aircraft Model at High Angles-of-attack (Short Communication), Defence Science Journal, vol.52, issue.4, p.417, 2002. ,
DOI : 10.14429/dsj.52.2199
Visualization and flow surveys of the leading edge vortex structure on delta wing planforms, 24th Aerospace Sciences Meeting, 1986. ,
DOI : 10.1063/1.862033
A concept of the vortex lift of sharp-edge delta wings based on a leading-edge suction analogy, 1966. ,
Application of the leading-edge suction analogy os vortex lift to the drag due to lift of sharp-edge Delta wings, 1968. ,
Predictions of vortex-lift characteristics by a leading-edge suctionanalogy, Journal of Aircraft, vol.67, issue.3, pp.193-199, 1971. ,
DOI : 10.1090/qam/17096
Predictions of vortex-lift characteristics based on a leading-edge suction analogy, 6th Annual Meeting and Technical Display, pp.69-1133, 1969. ,
DOI : 10.2514/6.1969-1133
Augmentation of inviscid airfoil theory to predict and model 2d unsteady vortex dominated flows, 41st AIAA Fluid Dynamics Conference and Exhibit, 2011. ,
Contrôle expérimental de l'écoulement tourbillonnaire sur une aile delta, 2004. ,
Etude et controle du decrochage d'ailes et gouvernes de missile en regime transsonique, 2009. ,
Sur la théorie de l'aile en delta. Tourbillon d'apex et nappes en cornet, 1956. ,
Flow over a Wing with an Attached Free Vortex, Studies in Applied Mathematics, vol.38, issue.2, pp.107-117, 1977. ,
DOI : 10.2514/3.60508
The aerodynamics of insect flight, Journal of Experimental Biology, vol.206, issue.23, pp.4191-4208, 2003. ,
DOI : 10.1242/jeb.00663
Transition Detection and Skin Friction Measurements on Rotating Propeller Blades, 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference, 2012. ,
DOI : 10.1063/1.1723300
Tip loss corrections for wind turbine computations, Wind Energy, vol.124, issue.4, pp.457-475, 2005. ,
DOI : 10.1002/we.153
URL : http://orbit.dtu.dk/en/publications/tip-loss-corrections-for-wind-turbine-computations(8877e882-4f59-4047-b116-8bda8e0d48d8).html
Tip Loss Correction for Actuator/Navier???Stokes Computations, Journal of Solar Energy Engineering, vol.124, issue.2, pp.209-213, 2005. ,
DOI : 10.1115/1.1850488
URL : http://orbit.dtu.dk/en/publications/tip-loss-correction-for-actuator--navier-stokes-computations(a444f235-6a1e-4e06-bfbe-a20d7b6879fb).html
The role of leading edge vortex flows in prop-fan interaction noise, AIAA 13th Aeroacoustics Conference, 1990. ,
Numerical simulation of vortex generation and capture above an airfoil, 31st Aerospace Sciences Meeting, p.864, 1993. ,
DOI : 10.2514/6.1993-864
Sectional prediction of lift coefficients on rotating wind turbine blades in stall, pp.93-052, 1994. ,
Etude expérimentale d'écoulements tourbillonnaires soumis à des effets de gradient de pression adverse, AGARD Symposium on Aerodynamics of Vortical Type Flows in Three Dimensions, 1983. ,
Large aerodynamic forces on a sweeping wing at low reynolds number, Acta Mechanica Sinica, vol.20, pp.24-31, 2004. ,
Insight into wind turbine stall and post-stall aerodynamics, Wind Energy, vol.7, issue.3, pp.247-260, 2004. ,
DOI : 10.1002/we.122
Reliable Force Predictions for a Flapping-Wing Micro Air Vehicle: A ???Vortex-Lift??? Approach, International Journal of Micro Air Vehicles, vol.149, issue.4, pp.201-215, 2011. ,
DOI : 10.1242/jeb.01266
URL : http://journals.sagepub.com/doi/pdf/10.1260/1756-8293.3.4.201
Low Aspect Ratio Aerodynamics at Low Reynolds Numbers, AIAA Journal, vol.75, issue.1, pp.865-873, 2004. ,
DOI : 10.2514/3.58681
The aerodynamics of revolving wings ii. propeller force coefficients from mayfly to quail, Journal of Experimental Biology, issue.11, pp.2051565-1576, 2002. ,
A Study of the Leading Edge Vortex and Tip Vortex on Prop-Fan Blades, Journal of Turbomachinery, vol.109, issue.3, 1987. ,
DOI : 10.1115/1.3262109
Modification des tourbillons d'extremite d'helices contra-rotatives en vue d'une reduction des nuisances sonores, Bibliography, 2013. ,
URL : https://hal.archives-ouvertes.fr/pastel-00843556
Counterrotating open rotor (cror) : flow physics and simulation, 20th French Mechanics Congress, 2011. ,
Wind tunnel investigations of vortex breakdown on slender sharp edged wings, 1968. ,
Vortex breakdown on slender sharp-edged wings, Journal of Aircraft, vol.8, issue.3, pp.156-161, 1971. ,
Etude experimentale, au tunnel hydrodynamique, de l'ecoulement autour de l'aile delta aux faibles vitesses, 1957. ,
Etude experimentale, au tunnel hydrodynamique, de l'eclatement des tourbillons d'apex d'une aile delta aux faibles vitesses, 1959. ,
Sur l'éclatement des tourbillons d'apex d'une aile delta aux faibles vitesses, La Recherche Aéronautique, p.74, 1960. ,
Tourbillons d'apex d'ailes tres minces, 1960. ,
Tourbillons d'apex d'ailes delta et gothiques epaisses, 1961. ,
Reassessment of the scale-determining equation for advanced turbulence models, AIAA Journal, vol.4, issue.3, pp.1299-1310, 1988. ,
DOI : 10.2514/6.1988-220
Parameter Variation and the Leading-Edge Vortex of a Rotating Flat Plate, AIAA Journal, vol.8, issue.4, pp.348-357, 2014. ,
DOI : 10.1002/sapm1977572107
Vorticity transport in the leading-edge vortex on a rotating blade, Journal of Fluid Mechanics, vol.743, pp.249-261, 2014. ,
DOI : 10.2514/3.12325
Contrarotating Open Rotor Operation for Improved Aerodynamics and Noise at Takeoff, Journal of Turbomachinery, vol.135, issue.3, 2013. ,
DOI : 10.1115/1.4006778
Aeroacoustic study of the interaction of a rotating blade with a batchelor vortex, 22nd AIAA/CEAS Aeroacoustics Conference, p.2999, 2016. ,
URL : https://hal.archives-ouvertes.fr/hal-01735830
Staggered upwind method for solving navier-stokes and turbulence model equations, AIAA journal, vol.33, issue.6, pp.991-998, 1995. ,
Influence of the aspect-ratio on the aerodynamics of the delta wings at high angle of attack, Journal of Aircraft, vol.25, issue.3, pp.200-205, 1988. ,