2011 Journal Article Thrust nozzle design study for a quasi-axisymmetric scramjet-powered vehicleTanimizu, K, Mee, DJ, Stalker, RJ and Jacobs, PA (2011). Thrust nozzle design study for a quasi-axisymmetric scramjet-powered vehicle. Journal of Propulsion and Power, 27 (1), 40-49. doi: 10.2514/1.48586 |
2010 Journal Article Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flowsKirchhartz, Rainer M., Paull, Allan, Mee, David J. and Olivier, Herbert (2010). Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flows. International Journal of Hypersonics, 1 (4), 199-208. doi: 10.1260/1759-3107.1.4.199 |
2010 Journal Article Attitude guidance for spinning vehicles with independent pitch and yaw controlCreagh, Michael and Mee, David (2010). Attitude guidance for spinning vehicles with independent pitch and yaw control. Journal of Guidance, Control and Dynamics, 33 (3), 915-922. doi: 10.2514/1.44430 |
2010 Journal Article Supersonic boundary-layer combustion: Effects of upstream entropy and shear-layer thicknessKirchhartz, R. M., Mee, D. J., Stalker, R. J., Jacobs, P. A. and Smart, M. K. (2010). Supersonic boundary-layer combustion: Effects of upstream entropy and shear-layer thickness. Journal of Propulsion and Power, 26 (1), 57-66. doi: 10.2514/1.44485 |
2009 Journal Article Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: Theory and experimentTanimizu, K, Mee, DJ, Stalker, RJ and Jacobs, PA (2009). Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: Theory and experiment. SHOCK WAVES, 19 (2), 83-93. doi: 10.1007/s00193-009-0194-x |
2009 Journal Article Boundary-layer separation due to combustion-induced pressure rise in a supersonic flowFrost, Myles A., Gangurde, Dhananjay Y., Paull, Allan and Mee, David J. (2009). Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow. AIAA Journal, 47 (4), 1050-1053. doi: 10.2514/1.40868 |
2008 Journal Article Effect of anti-scale agents on the solubility of CO2 in seawater at temperatures of 60 to 90oC and pressures of 1-2 barAl-Anezi, Khalid, Somerfield, Chris, Mee, David, Hankins, Nick and Hilal, Nidal (2008). Effect of anti-scale agents on the solubility of CO2 in seawater at temperatures of 60 to 90oC and pressures of 1-2 bar. Desalination, 227 (1-3), 46-56. doi: 10.1016/j.desal.2007.05.034 |
2008 Journal Article Parameters affecting the solubility of carbon dioxide in seawater at the conditions encountered in MSF desalination plantsAl-Anezi, Khalid, Somerfield, Chris, Mee, David and Hilal, Nidal (2008). Parameters affecting the solubility of carbon dioxide in seawater at the conditions encountered in MSF desalination plants. Desalination, 222 (1-3), 548-571. doi: 10.1016/j.desal.2007.01.128 |
2007 Journal Article New calibration technique for multiple-component stress wave force balancesAbdel-Jawad, Madhat M., Mee, David J. and Morgan, Richard G. (2007). New calibration technique for multiple-component stress wave force balances. Review of Scientific Instruments, 78 (6) 065101, 065101-1-065101-7. doi: 10.1063/1.2744235 |
2007 Journal Article Background oriented schlieren for flow visualisation in hypersonic impulse facilitiesRamanah, D., Raghunath, S., Mee, D. J., Rosgen, T. and Jacobs, P. A. (2007). Background oriented schlieren for flow visualisation in hypersonic impulse facilities. Shock Waves, 17 (1-2), 65-70. doi: 10.1007/s00193-007-0097-7 |
2007 Journal Article Boundary layers on a flat plate at suband superorbital speedsHayne, M.J., Mee, D.J., Gai, S.L. and McIntyre, T.J. (2007). Boundary layers on a flat plate at suband superorbital speeds. Journal of Thermophysics And Heat Transfer, 21 (4), 772-779. doi: 10.2514/1.26894 |
2006 Journal Article Reynolds analogy in high-enthalpy and high-Mach-number turbulent flowsSuraweera, M. V., Mee, D. J. and Stalker, R. J. (2006). Reynolds analogy in high-enthalpy and high-Mach-number turbulent flows. Aiaa Journal, 44 (4), 917-919. doi: 10.2514/1.18939 |
2006 Journal Article Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnelRobinson, M. J., Mee, D. J. and Paull, A. (2006). Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnel. Journal Of Propulsion And Power, 22 (1), 85-95. doi: 10.2514/1.15978 |
2005 Journal Article Scramjets and Shock Tunnels: The Queensland ExperienceStalker, R. J., Paull, A., Mee, D. J., Morgan, R. G. and Jacobs, P. A. (2005). Scramjets and Shock Tunnels: The Queensland Experience. Progress in Aerospace Sciences, 41 (6), 471-513. doi: 10.1016/j.paerosci.2005.08.002 |
2005 Journal Article Dynamic force balances for short-duration hypersonic testing facilitiesSahoo, N., Suryavamshi, K., Reddy, K. P. J. and Mee, D. J. (2005). Dynamic force balances for short-duration hypersonic testing facilities. Experiments In Fluids, 38 (5), 606-614. doi: 10.1007/s00348-005-0932-5 |
2004 Journal Article Rarefied, Superorbital Flows in an Expansion TubeWheatley, Vincent, Chiu, Sam Hsieh-Hsiang, Jacobs, Peter A., Macrossan, Michael N., Mee, David J. and Morgan, Richard G. (2004). Rarefied, Superorbital Flows in an Expansion Tube. International Journal for Numerical Methods for Heat and Fluid Flow, 14 (4), 512-537. doi: 10.1108/09615530410532277 |
2003 Journal Article Dynamic Calibration of Force Balances for Impulse Hypersonic FacilitiesMee, D. J. (2003). Dynamic Calibration of Force Balances for Impulse Hypersonic Facilities. Shock Waves, 12 (6), 443-455. doi: 10.1007/s00193-003-0181-6 |
2003 Journal Article Heat transfer and flow behind a step in high enthalpy superorbital flowHayne, MJ, Mee, DJ, Morgan, RG, Gai, SL and McIntyre, TJ (2003). Heat transfer and flow behind a step in high enthalpy superorbital flow. Aeronautical Journal, 107 (1073), 435-442. doi: 10.1017/s0001924000130040 |
2002 Journal Article Techniques for detailed heat transfer measurements in cold supersonic blowdown tunnels using thermochromic liquid crystalsMee, D. J., Chiu, H. S. and Ireland, P. T. (2002). Techniques for detailed heat transfer measurements in cold supersonic blowdown tunnels using thermochromic liquid crystals. International Journal of Heat And Mass Transfer, 45 (16), 3287-3297. doi: 10.1016/S0017-9310(02)00050-9 |
2002 Journal Article Thermochromic liquid crystals for assessing the performance of scramjet inlets with notched cowlsMee, David J., Skowronski, Michael D. and Chiu, H. H. Sam (2002). Thermochromic liquid crystals for assessing the performance of scramjet inlets with notched cowls. Journal of the Indian Institute of Science Section B: Physical and Chemical Sciences, 82 (3&4), 145-160. |