| The interaction of a shock wave with a laminar boundary layer at a compression corner in high-enthalpy flows including real gas effects SG Mallinson, SL Gai, NR Mudford Journal of fluid mechanics 342, 1-35, 1997 | 71 | 1997 |
| Free piston shock tunnels: developments and capabilities SL Gai Progress in Aerospace Sciences 29 (1), 1-41, 1992 | 65 | 1992 |
| Hypersonic fluid–structure interaction on a cantilevered plate with shock impingement GMD Currao, AJ Neely, CM Kennell, SL Gai, DR Buttsworth AIAA journal 57 (11), 4819-4834, 2019 | 59 | 2019 |
| Laminar near wake of a circular cylinder at hypersonic speeds G Park, SL Gai, AJ Neely AIAA journal 48 (1), 236-248, 2010 | 48 | 2010 |
| The effect of geometry on the base pressure recovery of segmented blunt trailing edges MS Petrusma, SL Gai Aeronautical Journal 98 (977), 267-274, 1994 | 45 | 1994 |
| Hypersonic transitional shock-wave–boundary-layer interaction on a flat plate GMD Currao, R Choudhury, SL Gai, AJ Neely, DR Buttsworth AIAA journal 58 (2), 814-829, 2020 | 43 | 2020 |
| Hypersonic compression corner flow with large separated regions SL Gai, A Khraibut Journal of Fluid Mechanics 877, 471-494, 2019 | 43 | 2019 |
| High-enthalpy, hypersonic compression corner flow SG Mallinson, SL Gai, NR Mudford AIAA journal 34 (6), 1130-1137, 1996 | 37 | 1996 |
| Supersonic flow over a shallow open rectangular cavity SL Gai, H Kleine, AJ Neely Journal of Aircraft 52 (2), 609-616, 2015 | 35 | 2015 |
| Measurements of heat transfer in separated highenthalpy dissociated laminar hypersonic flow behind a step SL Gai, NT Reynolds, C Ross, JP Baird Journal of Fluid Mechanics 199, 541-561, 1989 | 32 | 1989 |
| Mole-fraction-sensitive imaging of hypermixing shear layers JS Fox, AFP Houwing, PM Danehy, MJ Gaston, NR Mudford, SL Gai Journal of propulsion and power 17 (2), 284-292, 2001 | 30 | 2001 |
| Laminar heat transfer to blunt cones in high-enthalpy hypervelocity flows SL Gai, WS Joe Journal of thermophysics and heat transfer 6 (3), 433-438, 1992 | 30 | 1992 |
| Stagnation point heat flux in hypersonic high enthalpy flow SL Gai, NR Mudford Shock Waves 2 (1), 43-47, 1992 | 30 | 1992 |
| A method for the accurate determination of the thermal product (ρck) 1/2 for thin film heat transfer or surface thermocouple gauges PRA Lyons, SL Gai Journal of Physics E: Scientific Instruments 21 (5), 445, 1988 | 27 | 1988 |
| Laminar hypersonic leading edge separation–a numerical study A Khraibut, SL Gai, LM Brown, AJ Neely Journal of Fluid Mechanics 821, 624-646, 2017 | 24 | 2017 |
| Hypersonic fluid-structure interaction on a cantilevered plate GM Currao, AJ Neely, DR Buttsworth, SL Gai 7th European Conference for Aeronautics and Space Sciences 12, 13, 2017 | 24 | 2017 |
| Base flow of circular cylinder at hypersonic speeds G Park, SL Gai, AJ Neely AIAA Journal 54 (2), 458-468, 2016 | 22 | 2016 |
| Simulations of hypersonic, high-enthalpy separated flow over a'tick'configuration JN Moss, S O'Byrne, NR Deepak, SL Gai AIP Conference Proceedings 1501 (1), 1453-1460, 2012 | 22 | 2012 |
| Establishment of steady separated flow over a compression–corner in a free–piston shock tunnel SG Mallinson, SL Gai, NR Mudford Shock Waves 7 (4), 249-253, 1997 | 22 | 1997 |
| The boundary layer on a flat plate in hypervelocity flow SG Mallinson, SL Gai, NR Mudford The Aeronautical Journal 100 (994), 135-141, 1996 | 21 | 1996 |
