S. J. Barker and S. C. Crow, The motion of twodimensional vortex pairs in a ground effect, Journal of Fluid Mechanics, vol.82, issue.4, pp.659-671, 1977.

M. Bloxham, J. Bons, and R. Hollis, Horseshoe vortex control with leading edge endwall boundary layer removal, 4th Flow Control Conference, p.4319, 2008.

D. Borello, K. Hanjalic, and F. Rispoli, Computation of tip-leakage flow in a linear compressor cascade with a second-moment turbulence closure, International Journal of Heat and Fluid Flow, vol.28, issue.4, pp.587-601, 2007.

H. Brandt, L. Fottner, H. Saathoff, and U. Stark, Effects of the inlet flow conditions on the tip clearance flow of an isolated compressor rotor, ASME Turbo Expo, pp.1123-1132, 2002.

P. Chassaing, J. Decaix, G. Balarac, M. Dreyer, M. Farhat et al., Rans and les computations of the tip-leakage vortex for different gap widths, Journal of Turbulence, vol.16, pp.309-341, 2010.

J. Denton, Loss mechanisms in turbomachines, ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, pp.2-14, 1993.

W. J. Devenport and R. L. Simpson, Time-dependent and time-averaged turbulence structure near the nose of a wing-body junction, Journal of Fluid Mechanics, vol.210, pp.23-55, 1990.

A. Doukelis, K. Mathioudakis, K. Papailiou, K. Mathioudakis, and K. Papailiou, The effect of tip clearance gap size and wall rotation on the performance of a high-speed annular compressor cascade, ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition, pp.1-01, 1998.

R. Fearn and R. P. Weston, Vorticity associated with a jet in a cross flow, AIAA Journal, vol.12, issue.12, pp.1666-1671, 1974.

O. Flachsbart, Spaltverluste an Tragflügeln. ZAMM-Journal of Applied Mathematics and Mechanics/Zeitschrift für Angewandte Mathematik und Mechanik, vol.11, issue.6, pp.411-414, 1931.

M. Hasan, M. Casarella, and E. Rood, An experimental study of the flow and wall pressure field around a wing-body junction, vol.108, pp.308-314, 1986.

F. Heyes, H. Hodson, and G. Dailey, The effect of blade tip geometry on the tip leakage flow in axial turbine cascades, Journal of Turbomachinery, vol.114, issue.3, pp.643-651, 1992.

H. Hu and Z. Yang, An experimental study of the laminar flow separation on a low-reynolds-number airfoil, Journal of Fluids Engineering, vol.130, issue.5, p.51101, 2008.

M. Inoue and M. Kuroumaru, Structure of tip clearance flow in an isolated axial compressor rotor, Journal of Turbomachinery, vol.111, issue.3, pp.250-256, 1989.

M. Jacob, J. Grilliat, R. Camussi, C. Gennaro, and G. , Aeroacoustic investigation of a single airfoil tip leakage flow, International Journal of Aeroacoustics, 2010.
URL : https://hal.archives-ouvertes.fr/hal-00566045

L. Jacquin, Phenomenological description and simplified modelling of the vortex wake issuing from a jet in a cross flow, La Recherche Aérospatiale, vol.2, pp.117-133, 1994.

H. L. Julien, W. Kays, and R. Moffat, The turbulent boundary layer on a porous plate-an experimental study of the effects of a favorable pressure gradient, 1969.

F. Kameier and W. Neise, Experimental study of tip clearance losses and noise in axial turbomachines and their reduction, Journal of Turbomachinery, vol.119, issue.3, pp.460-471, 1997.

S. Kang and C. Hirsch, Experimental study on the three-dimensional flow within a compressor cascade with tip clearance: Part Ivelocity and pressure fields, Journal of Turbomachinery, vol.115, issue.3, pp.435-443, 1993.

S. Kang and C. Hirsch, Numerical simulation of threedimensional viscous flow in a linear compressor cascade with tip clearance, Journal of Turbomachinery, vol.118, issue.3, pp.492-502, 1996.

A. R. Karagozian, The jet in crossflow, Physics of Fluids, vol.26, issue.10, p.101303, 2014.

B. Lakshminarayana and J. H. Horlock, Tip-clearance flow and losses for an isolated compressor blade, 1963.

F. R. Menter, Two-equation eddy-viscosity turbulence models for engineering applications, AIAA Journal, vol.32, issue.8, pp.1598-1605, 1994.

C. B. Millikan, Aerodynamics of the Airplane, Courier, 2018.

J. Moore and J. Tilton, Tip leakage flow in a linear turbine cascade, Journal of Turbomachinery, vol.110, issue.1, pp.18-26, 1988.

C. Muthanna and W. Devenport, Wake of a compressor cascade with tip gap, part 1: Mean flow and turbulence structure, AIAA Journal, vol.42, issue.11, pp.2320-2331, 2004.

S. B. Pope, Turbulent flows, 2011.
URL : https://hal.archives-ouvertes.fr/hal-00712179

T. Praisner and C. Smith, The dynamics of the horseshoe vortex and associated endwall heat transfer. Part I: Temporal behavior, Journal of Turbomachinery, vol.128, issue.4, pp.747-754, 2006.

, Prandtl L (1919) Tragflügeltheorie. II. Mitteilung. Nachrichten von der Gesellschaft der Wissenschaften zu Göttingen, Mathematisch-Physikalische Klasse pp, pp.107-137

D. A. Rains, Tip clearance flow induced endwall boundary layer separation in a single-stage axial-flow low-speed compressor, p.501, 1954.

G. Smith and N. A. Cumpsty, Flow phenomena in compressor casing treatment, Journal of Turbomachinery, vol.113, issue.2, pp.252-259, 1982.

J. Storer and N. Cumpsty, An approximate analysis and prediction method for tip clearance loss in axial compressors, Journal of Turbomachinery, vol.116, issue.4, pp.648-656, 1994.

H. D. Vo, C. S. Tan, and E. M. Greitzer, Criteria for spike initiated rotating stall, Journal of Turbomachinery, vol.130, issue.1, p.11023, 2008.

J. Z. Wu, H. Y. Ma, M. Zhou, T. Anor, H. Liu et al., Direct numerical simulation of turbulent flow around a wallmounted cube: spatio-temporal evolution of largescale vortices, Springer Science & Business Media Yakhot A, vol.566, pp.1-9, 2006.