| Scramjets and shock tunnels—the Queensland experience RJ Stalker, A Paull, DJ Mee, RG Morgan, PA Jacobs Progress in Aerospace Sciences 41 (6), 471-513, 2005 | 150 | 2005 |
| An examination of the contributions to loss on a transonic turbine blade in cascade DJ Mee, NC Baines, MLG Oldfield, TE Dickens | 124 | 1992 |
| Dynamic calibration of force balances for impulse hypersonic facilities DJ Mee Shock Waves 12, 443-455, 2003 | 114 | 2003 |
| Numerical investigations of flow and energy fields near a thermoacoustic couple H Ishikawa, DJ Mee The Journal of the Acoustical Society of America 111 (2), 831-839, 2002 | 99 | 2002 |
| Three-component force balance for flows of millisecond duration DJ Mee, WJT Daniel, JM Simmons AIAA journal 34 (3), 590-595, 1996 | 98 | 1996 |
| Boundary-layer transition measurements in hypervelocity flows in a shock tunnel DJ Mee AIAA journal 40 (8), 1542-1548, 2002 | 97 | 2002 |
| Experiments on supersonic combustion ramjet propulsion in a shock tunnel A Paull, RJ Stalker, DJ Mee Journal of Fluid Mechanics 296, 159-183, 1995 | 88 | 1995 |
| Numerical modelling of the self-heating process of a wet porous medium A Ejlali, DJ Mee, K Hooman, BB Beamish International Journal of Heat and Mass Transfer 54 (25-26), 5200-5206, 2011 | 81 | 2011 |
| Design, modelling and analysis of a six component force balance for hypervelocity wind tunnel testing AL Smith, DJ Mee, WJT Daniel, T Shimoda Computers & Structures 79 (11), 1077-1088, 2001 | 64 | 2001 |
| Suitability of the k–ω turbulence model for scramjet flowfield simulations WYK Chan, PA Jacobs, DJ Mee International Journal for Numerical Methods in Fluids 70 (4), 493-514, 2012 | 62 | 2012 |
| Uncertainty analysis of conditions in the test section of the T4 shock tunnel DJ Mee | 62 | 1993 |
| Skin friction reduction in hypersonic turbulent flow by boundary layer combustion M Suraweera, D Mee, R Stalker 43rd AIAA Aerospace Sciences Meeting and Exhibit, 613, 2005 | 57 | 2005 |
| Background oriented schlieren for flow visualisation in hypersonic impulse facilities D Ramanah, S Raghunath, DJ Mee, T Rösgen, PA Jacobs Shock waves 17, 65-70, 2007 | 54 | 2007 |
| Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow MA Frost, DY Gangurde, A Paull, DJ Mee AIAA journal 47 (4), 1050-1053, 2009 | 47 | 2009 |
| Dynamic force balances for short-duration hypersonic testing facilities N Sahoo, K Suryavamshi, KPJ Reddy, DJ Mee Experiments in Fluids 38, 606-614, 2005 | 44 | 2005 |
| Three-component force measurements on a large scramjet in a shock tunnel MJ Robinson, DJ Mee, CY Tsai, RJ Bakos Journal of spacecraft and rockets 41 (3), 416-425, 2004 | 42 | 2004 |
| Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10 LJ Doherty, MK Smart, DJ Mee AIAA Journal 53 (11), 3196-3207, 2015 | 41 | 2015 |
| Drag measurements at Mach 5 using a stress wave force balance SL Tuttle, DJ Mee, JM Simmons Experiments in Fluids 19 (5), 336-341, 1995 | 39 | 1995 |
| Free piston shock tunnels HEG, HIEST, T4 and T5 K Hannemann, K Itoh, DJ Mee, HG Hornung Experimental Methods of Shock Wave Research, 181-264, 2016 | 36 | 2016 |
| Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnel MJ Robinson, DJ Mee, A Paull Journal of Propulsion and Power 22 (1), 85-95, 2006 | 34 | 2006 |
