| Shock wave-boundary-layer interactions H Babinsky, JK Harvey Cambridge University Press, 2011 | 836 | 2011 |
| Microramp control of supersonic oblique shock-wave/boundary-layer interactions H Babinsky, Y Li, CWP Ford AIAA journal 47 (3), 668-675, 2009 | 332 | 2009 |
| Lift and the leading-edge vortex CWP Ford, H Babinsky Journal of fluid mechanics 720, 280-313, 2013 | 253 | 2013 |
| How do wings work? H Babinsky Physics Education 38 (6), 497, 2003 | 153 | 2003 |
| Shock-wave/boundary-layer interaction control using three-dimensional bumps for transonic wings H Ogawa, H Babinsky, M Pätzold, T Lutz AIAA journal 46 (6), 1442-1452, 2008 | 135 | 2008 |
| Effect of microvortex generators on seperated normal shock/boundary layer interactions H Holden, H Babinsky Journal of Aircraft 44 (1), 170-174, 2007 | 128 | 2007 |
| Normal shock boundary layer control with various vortex generator geometries S Lee, E Loth, H Babinsky Computers & Fluids 49 (1), 233-246, 2011 | 122 | 2011 |
| Unsteady shock wave dynamics PJK Bruce, H Babinsky Journal of Fluid Mechanics 603, 463-473, 2008 | 120 | 2008 |
| SBLI control for wings and inlets H Babinsky, H Ogawa Shock Waves 18, 89-96, 2008 | 117 | 2008 |
| Corner effect and separation in transonic channel flows PJK Bruce, DMF Burton, NA Titchener, H Babinsky Journal of Fluid Mechanics 679, 247-262, 2011 | 109 | 2011 |
| Corner separation effects for normal shock wave/turbulent boundary layer interactions in rectangular channels DMF Burton, H Babinsky Journal of Fluid Mechanics 707, 287-306, 2012 | 100 | 2012 |
| Unsteady lift generation on rotating wings at low Reynolds numbers AR Jones, H Babinsky Journal of Aircraft 47 (3), 1013-1021, 2010 | 98 | 2010 |
| Shock wave/boundary-layer interaction control using a combination of vortex generators and bleed N Titchener, H Babinsky AIAA journal 51 (5), 1221-1233, 2013 | 94 | 2013 |
| A review of the use of vortex generators for mitigating shock-induced separation N Titchener, H Babinsky Shock Waves 25, 473-494, 2015 | 91 | 2015 |
| Reynolds number effects on leading edge vortex development on a waving wing AR Jones, H Babinsky Experiments in fluids 51 (1), 197-210, 2011 | 90 | 2011 |
| On the development and early observations from a towing tank-based transverse wing–gust encounter test rig SJ Corkery, H Babinsky, JK Harvey Experiments in Fluids 59, 1-16, 2018 | 79 | 2018 |
| Unsteady effects of shock wave induced separation P Doerffer, C Hirsch, JP Dussauge, H Babinsky, GN Barakos Springer Science & Business Media, 2010 | 75 | 2010 |
| Assessment of computational fluid dynamics and experimental data for shock boundary-layer interactions JR DeBonis, WL Oberkampf, RT Wolf, PD Orkwis, MG Turner, H Babinsky, ... AIAA journal 50 (4), 891-903, 2012 | 71 | 2012 |
| A combined experimental and numerical study of flow structures over three-dimensional shock control bumps WS Wong, N Qin, N Sellars, H Holden, H Babinsky Aerospace Science and Technology 12 (6), 436-447, 2008 | 65 | 2008 |
| Vortical structures on three-dimensional shock control bumps SP Colliss, H Babinsky, K Nübler, T Lutz AIAA Journal 54 (8), 2338-2350, 2016 | 63 | 2016 |
