A. Abbas, J. de Vicente, E. Valero, Aerodynamic technologies to improve aircraft performance, Aerospace Science and Technology, 2013, 28, 100–132. CrossRef
	M.L. Post, T. C. Corke, Separation Control on high angle of attack airfoil using plasma actuators, AIAA Journal, 2004, 42, 2177–2184. CrossRef
	J.C. Lin, F.G. Howard, G.V. Selby, Turbulent flow separation control through passive techniques, AIAA paper, 1989, 976.
	H. Babinsky, Y. Li, C. W. Pitt Ford, Microramp control of supersonic oblique shock-wave/boundary-layer interactions, AIAA Journal, 2009, 47, 668–675. CrossRef
	J.C. Lin, Control of turbulent boundary-layer separation using micro-vortex generators, AIAA paper, 1999, 3404.
	K. S. Bohannon, Passive flow control on civil aircraft flaps using sub-boundary layer vortex generators in the AWIATOR programme, AIAA Paper, 2006, 2858.
	H. Babinsky, N. Makinson, C. Morgan, Micro-vortex generator for supersonic engine inlets, AIAA paper, 2007, 521.
	G.E. Elsinga, F. Scarano, B. Wieneke, B.W. van Oudheusden, Tomographic particle image velocimetry, Experiments in Fluids, 2006, 41, 933–947. CrossRef
	G.-S. Jiang, C.-W. Shu, Efficient Implementation of Weighted ENO Schemes, Journal of Computational Physics, 1996, 126, 202–228. CrossRef
	D.M. Rao, T.T. Kariya, Boundary-layer submerged vortex generators for separation control – an exploratory study, AIAA paper, 1988, 3546.
	H.D. Taylor, The elimination of diffuser separation by vortex generators. United Aircraft Corporation Report, 1947, No.R-4012-3.
	A.E. Holmes, P. K. Hickey, W. R. Murphy, D. A. Hilton, The application of sub-boundary layer vortex generators to reduce canopy “Mach rumble” interior noise on the Gulfstream III, AIAA paper, 1987, 84.
	S. Lee, E. Loth, Supersonic boundary-layer interactions with various micro-vortex generator geometries, Aeronautical Journal, 2009, 113, 683–697.
	H. Holden, H. Babinsky, Effects of microvortex generators on the separated normal shock/boundary layer interactions, Journal of Aircraft, 2007, 44, 170–174. CrossRef
	C.S. Yao, J.C. Lin, B.G. Allan, Flow-field measurement of embedded streamwise vortex generated from passive flow-control devices, International Journal of Flow Control, 2009, 1, 255–270. Abstract
	A. M. Kuethe, Effect of streamwise vortices on wake properties associated with sound generation, Journal of Aircraft, 1972, 9, 715–719. CrossRef
	S. Lee, E. Loth, Impact of ramped vanes on normal shock boundary-layer interaction, AIAA Journal, 2012, 50, 2069–2079. CrossRef
	J.C. Lin, G.V. Selby, F. G. Howard, Exploratory study of vortex-generating devices for turbulent flow separation control, AIAA paper, 1991, 42.
	Y. Yan, Q. Li, C. Liu, F. K. Lu, Numerical, experimental and theoretical studies on mechanism of K-H instability and ring generation behind supersonic MVG, AIAA paper, 2011, 676.
	Z. Sun, F. F. J. Schrijer, B. W. van Oudheusden, The three-dimensional flow organization past a micro-ramp in a supersonic boundary layer, Physics of Fluids, 2012, 24, 055105. CrossRef
	W. R. Nolan, H. Babinsky, Characterization of micro-vortex generators in supersonic flows, AIAA paper, 2011, 71.
	T. Herges, E. Kroeker, G. Elliott, C. Dutton, Microramp flow control of normal shock/boundary-layer interactions, AIAA Journal, 2010, 48, 2529–2542. CrossRef
	Z. Sun, F. F. J. Schrijer, F. Scarano, B. W. van Oudheusden, Decay of the supersonic turbulent wakes from micro-ramps, Physics of Fluids, 2014, 26, 025115. CrossRef
	F. K. Lu, A. J. Pierce, Y. Shih, Experimental study of near wake of micro vortex generators in supersonic flow, AIAA Paper, 2010, 4623.
	M. R. Saad, A. Che Idris, H. Zare-Behtash, K. Kontis, Micro-ramps in Mach 5 hypersonic flow, AIAA Paper, 2012, 676.
	J. W. Miles, On the generation of surface waves by shear flows Part 3. Kelvin-Helmholtz instability, Journal of Fluid Mechanics, 1959, 6, 583–598. CrossRef
	Y. Zhao, S. Yi, L. Tian, Z. Chen, Supersonic flow imaging via nanoparticles, Science in China Series E: Technological Sciences, 2009, 52, 3640–3648. CrossRef
	D. P. Wang, Z. X. Xia, Y. X. Zhao, Q. H. Wang, B. Liu, Vortical structures of supersonic flow over a delta-wing on a flat plate, Applied Physics Letters, 2013, 102, 061911. CrossRef
	Q. Li, C. Liu, LES for supersonic ramp control flow using MVG at M = 2.5 and Re0 = 1440, AIAA Paper, 2010, 592.
	P. L. Blinde, R. A. Humble, B. W. van Oudheusden, F. Scarano, Effects of micro-ramps on a shock wave/turbulent boundary layer interaction, Shock Waves, 2009, 19, 507–520. CrossRef
	D. Xue, Z. Chen, X. Jiang, B. Fan, Numerical investigations on the wake structures of micro-ramp and micro-vanes, Fluid Dynamics Research, 2014, 46, 015505. CrossRef
	Q. Li, C. Liu, Implicit LES for supersonic microramp vortex generator: new discovery and new mechanisms, Modelling and Simulation in Engineering, 2011, 2011, 1–15.
	Z. Sun, F. Scarano, B. W. van Oudheusden, F. F. J. Schrijer, Y. Yan, C. Liu, Numerical and experimental investigations of the supersonic microramp wake, AIAA Journal, 2014, 52, 1518–1527. CrossRef
	P. R. Ashill, J. L. Fulker, K. C. Hackett, Research at DERA on sub boundary layer vortex generators, AIAA Paper, 2001, 887.
	T. C. Tai, Effect of midwing vortex generators on V-22 aircraft forward-flight aerodynamics, Journal of Aircraft, 2003, 40, 623–630. CrossRef
	A. E. Holmes, P. K. Hickey, W. R. Murphy, D. A. Hilton, The application of sub-boundary layer vortex generators to reduce canopy “Mach rumble” interior noise on the Gulfstream III, AIAA Paper, 1987, 84.
	J. P. Dussauge, P. Dupont, J.-F. Debiève, Unsteadiness in shock wave boundary layer interactions with separation, Aerospace Science and Technology, 2006, 10, 85–91. CrossRef
	R. A. Humble, Unsteady flow organization of a shock wave/boundary layer interaction, Doctoral thesis, Delft University of Technology, 2009.
	J. Delery, J. P. Dussauge, Some physical aspects of shock wave/boundary layer interactions, Shock waves, 2009, 19, 453–468. CrossRef
	M. C. Galbraith, P. D. Orkwis, J. A. Benek, Multi-row micro-ramp actuators for shock wave boundary-layer interaction control, AIAA Paper, 2009, 321.
	S. Ghosh, J. I. Choi, J. Edwards, Numerical simulations of effects of micro vortex generators using immersed-boundary methods, AIAA Journal, 2010, 48, 92–103. CrossRef
	P. R. Ashill, J. L. Fulker, K. C. Hackett, Studies of flows induced by sub boundary layer vortex generators (SBVGs), AIAA Paper, 2002, 968.
	W. Bo, L. Weidong, Z. Yuxin, F. Xiaoqiang, W. Chao, Experimental investigation of the micro-ramp based shock wave and turbulent boundary layer interaction control, Physics of Fluids, 2012, 24, 055110. CrossRef
	B. H. Anderson, H. Tinapple, L. Surber, Optimal control of shock wave turbulent boundary layer interactions using micro array actuation, AIAA Paper, 2006, 3197.
	S. M. Hirt, B. H. Anderson, Experimental investigation of the application of microramp flow control to an oblique shock interaction, AIAA Paper, 2009, 919.
	P. Doerffer, C. Hirsch, J. P. Dussauge, H. Babinsky, G. N. Barakos, Unsteady effects of shock wave induced separation, Notes on numerical fluid mechanics and multidisciplinary design, vol. 114, Spinger, 2011.
	H. Babinsky, N. Makinson, C. Morgan, Micro-vortex generator for supersonic engine inlets, AIAA Paper, 2007, 521.
	N. Titchener, H. Babinsky, Microvortex generators applied to flow field containing a normal shock wave and diffuser, AIAA Journal, 2011, 49, 1046–1056. CrossRef
	M. Rybalko, H. Babinsky, E. Loth, Vortex generators for a normal shock/boundary layer interaction with a downstream diffuser, Journal of Propulsion Power, 2012, 28, 71–82. CrossRef
	S. Lee, E. Loth & H. Babinsky, Normal shock boundary layer control with various vortex generator geometries, Computers & Fluids, 2011, 49, 233–246. CrossRef
	T. Herges, G. Elliott, C. Dutton, Y. Lee, Micro-vortex generators and recirculating flow control of normal shock stability and position sensitivity, AIAA Paper, 2010, 1097.
	S. B. Verma, C. Manisankar, C. Raju, Control of shock unsteadiness in shock boundary-layer interaction on a compression corner using mechanical vortex generators, Shock waves, 2012, 22, 327–339. CrossRef
	Q. Li, Y. Yan, X. Wang, C. Liu, The interaction between vortex rings and oblique shocks by the MVG controlled ramp flow at M = 2.5, AIAA Paper, 2011, 861.