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2010

Journal Article

Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flows

Kirchhartz, 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

Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flows

2010

Journal Article

Attitude guidance for spinning vehicles with independent pitch and yaw control

Creagh, 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

Attitude guidance for spinning vehicles with independent pitch and yaw control

2010

Journal Article

Supersonic boundary-layer combustion: Effects of upstream entropy and shear-layer thickness

Kirchhartz, 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

Supersonic boundary-layer combustion: Effects of upstream entropy and shear-layer thickness

2009

Journal Article

Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: Theory and experiment

Tanimizu, 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

Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: Theory and experiment

2009

Journal Article

Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow

Frost, 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

Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow

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 bar

Al-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

Effect of anti-scale agents on the solubility of CO2 in seawater at temperatures of 60 to 90oC and pressures of 1-2 bar

2008

Journal Article

Parameters affecting the solubility of carbon dioxide in seawater at the conditions encountered in MSF desalination plants

Al-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

Parameters affecting the solubility of carbon dioxide in seawater at the conditions encountered in MSF desalination plants

2007

Journal Article

New calibration technique for multiple-component stress wave force balances

Abdel-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

New calibration technique for multiple-component stress wave force balances

2007

Journal Article

Background oriented schlieren for flow visualisation in hypersonic impulse facilities

Ramanah, 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

Background oriented schlieren for flow visualisation in hypersonic impulse facilities

2007

Journal Article

Boundary layers on a flat plate at suband superorbital speeds

Hayne, 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

Boundary layers on a flat plate at suband superorbital speeds

2006

Journal Article

Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnel

Robinson, 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

Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnel

2006

Journal Article

Reynolds analogy in high-enthalpy and high-Mach-number turbulent flows

Suraweera, 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

Reynolds analogy in high-enthalpy and high-Mach-number turbulent flows

2005

Journal Article

Scramjets and Shock Tunnels: The Queensland Experience

Stalker, 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

Scramjets and Shock Tunnels: The Queensland Experience

2005

Journal Article

Dynamic force balances for short-duration hypersonic testing facilities

Sahoo, 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

Dynamic force balances for short-duration hypersonic testing facilities

2004

Journal Article

Rarefied, Superorbital Flows in an Expansion Tube

Wheatley, 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

Rarefied, Superorbital Flows in an Expansion Tube

2003

Journal Article

Heat transfer and flow behind a step in high enthalpy superorbital flow

Hayne, 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

Heat transfer and flow behind a step in high enthalpy superorbital flow

2003

Journal Article

Dynamic Calibration of Force Balances for Impulse Hypersonic Facilities

Mee, 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

Dynamic Calibration of Force Balances for Impulse Hypersonic Facilities

2002

Journal Article

Techniques for detailed heat transfer measurements in cold supersonic blowdown tunnels using thermochromic liquid crystals

Mee, 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

Techniques for detailed heat transfer measurements in cold supersonic blowdown tunnels using thermochromic liquid crystals

2002

Journal Article

Thermochromic liquid crystals for assessing the performance of scramjet inlets with notched cowls

Mee, 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.

Thermochromic liquid crystals for assessing the performance of scramjet inlets with notched cowls

2002

Journal Article

Boundary-layer transition measurements in hypervelocity flows in a shock tunnel

Mee, D. J. (2002). Boundary-layer transition measurements in hypervelocity flows in a shock tunnel. AIAA Journal, 40 (8), 1542-1548. doi: 10.2514/2.1851

Boundary-layer transition measurements in hypervelocity flows in a shock tunnel