Professor David Mee

Professor

School of Mechanical and Mining Engineering
Faculty of Engineering, Architecture and Information Technology
d.mee@uq.edu.au
+61 7 336 54058

Overview

Prof David Mee's research interests are in Hypersonic and Supersonic Flow.

After completing his PhD at UQ, he spent five years as a Research Fellow in the turbomachinery research group at Oxford University in the U.K. He returned to UQ as an ARC Queen Elizabeth II Research Fellow in 1991 and joined the academic staff of the Department of Mechanical Engineering in 1993. He served as Head of the Division of Mechanical Engineering from 2007 to 2017, acting Head of the School of Engineering from January to July 2009 and Head of the School of Mechanical and Mining Engineering from 2009 to 2017.

David has a strong research record in the field of hypersonics aerothermodynamics. He is recognised worldwide for his work on rapid response force balances, which are essential technology for categorising the performance of scramjet engines in transient facilities, such as our shock tubes. He was a member of the team that conducted the first known wind-tunnel test in which a scramjet vehicle produced net thrust.

He has pioneered the use of stress wave force balances for measurement of multiple components of force on scramjet-powered vehicles and the techniques are in use around the world.

Research Interests

  • Superorbital Flows with Separation
    This project is directed towards the influence that real gas effects may have on separation regions in superorbital hypersonic flows.
  • Boundary-layer combustion
    Injection, ignition and combustion of fuel into the boundary layer of a supersonic flow can lead to substantial reductions in skin friction. This has potential for improvement of the performance of scramjet-powered vehicles.
  • Force Measurement in Impulse Facilities
    Measurement of aerodynamic forces on bodies in short-duration impulse facilities. A number of such facilities exist at The University of Queensland.
  • Scramjet Testing in Shock Tunnels
    Generally half the drag of hypersonic vehicles will be caused by air friction on the aircraft�s skin. A new method of reducing skin friction has been discovered. The range of conditions under which this method will be effective are being investigated.
  • Boundary-layer Transition
    This project studies the processes by which a laminar boundary layer transitions to a turbulent one under conditions of hypervelocity flow. This will lead to a better understanding and improved modelling of the high-speed transition process.

Qualifications

  • PhD, The University of Queensland
  • Bachelor of Engineering (Mech), The University of Queensland

Publications

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Supervision

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Publications

Book Chapter

  • Hannemann, Klaus, Itoh, Katsuhiro, Mee, David J. and Hornung, Hans G. (2016). Free piston shock tunnels HEG, HIEST, T4 and T5. In Hans Grönig, Yasuyuki Horie and Kazuyoshi Takayama (Ed.), Experimental methods of shock wave research (pp. 181-264) London, United Kingdom: Springer International Publishing. doi:10.1007/978-3-319-23745-9_7

Journal Article

Conference Publication

  • Raghunath, Sreekanth , Narasimha, Roddam and Mee, David J. (2017). Dependence of Turbulent Spot Initiation Rates on Hypersonic Boundary Layer Flow Parameters. In: 55th AIAA Aerospace Sciences Meeting and Exhibit, Dallas, TX, United States, (). 9-13 January 2017. doi:10.2514/6.2017-1684

  • Mee, D. J. and Raghunath, S. (2016). Boundary layer transition in hypersonic flows. In: Franco-Australian Symposium on Hypersonics and High Enthalpy Flows, Châtenay-Malabry, France, (). 7-9 September 2016.

  • Mee, D. J. (2016). Force measurement in impulse hypersonic facilities. In: First International Symposium on Hypersonics, Daejeon, South Korea, (). 27-30 November 2016.

  • Basore, K. D., Selzer, M., Wheatley, V., Boyce, R. R., Mee, D. J., Capra, B. R., Kuhn, M. and Brieschenk, S. (2016). Performance Comparison of Distributed Injection Methods for Hypersonic Film-Cooling. In: Proceedings of 20th Australasian Fluid Mechanics Conference. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, (). 5-8 December 2016.

  • Mee, D. J. and Raghunath, S. (2016). UQ research in transitional flows. In: 1st French-Australian Workshop on Re-entry and Hypersonic Aerothermodynamics, Brisbane, QLD, Australia, (). 23-25 February 2016.

  • Doherty, Luke J., Smart, Michael K. and Mee, David J. (2015). Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10. In: AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, United States, (3196-3207). 16– 20 June 2014. doi:10.2514/1.J053785

  • Mee, David J. and Vallis, Jack (2015). Improving sound diffusion in a reverberation chamber. In: Australian Acoustical Society. Acoustics 2015, Hunter Valley, Australia, (). 15-18 November 2015.

  • Doherty, Luke J., Smart, Michael K. and Mee, David J. (2015). Measurement of three-components of force on an airframe integrated scramjet at Mach 10. In: 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, (). 6-9 July 2015. doi:10.2514/6.2015-3523

  • Mee, D. J. and Tanguy, G. (2015). Turbulent spot initiation rates in boundary layers in a shock tunnel. In: Riccardo Bonazza and Devesh Ranjan, Proceedings of the 29th International Symposium on Shock Waves (ISSW29). International Symposium on Shock Waves, Madison, WI, United States, (623-628). 14-19 July 2013. doi:10.1007/978-3-319-16835-7_99

  • Doherty, Luke J., Smart, Michael K. and Mee, David J. (2014). Experimental testing of an airframe integrated 3-D scramjet at true mach 10 flight conditions. In: AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014, Atlanta, GA, United States, (). 16-20 June 2014. doi:10.2514/MHYTASP14

  • Bateup, Mark L., Paull, Allan and Mee, David J. (2013). Ethylene augmentation of JP-8+100 in a supersonic combustor. In: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2013: Proceedings. JPC 2013: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, United States, (1164-1173). 14-17 July, 2013. doi:10.2514/6.2013-3700

  • Doherty, Luke J., Smart, Michael K. and Mee, David J. (2012). Design of an airframe integrated 3-D scramjet and experimental results at a Mach 10 flight condition. In: Proceedings of the 18th AIAA/3AF International Space Planes and Hypersonics Systems and Technologies Conference. 18th AIAA/3AF International Space Planes and Hypersonics Systems and Technologies Conference, Tours, France, (1-17). 24 - 28 September 2012. doi:10.2514/6.2012-5910

  • Wilson Chan, Mee, David J., Smart, Michael K. and Turner, James J. (2012). Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion. In: Proceedings of the 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, (1-16). 24-28 September 2012. doi:10.2514/6.2012-5889

  • Creagh, Michael A. and Mee, David J. (2011). Attitude guidance and control for a spinning, asymmetrical rocket payload. In: AIAC14 Fourteenth Australian International Aerospace Congress. AIAC14 Fourteenth Australian International Aerospace Congress, Melbourne, Australia, (). 28 February - 3 March 2011.

  • Hayne, M. J., Taylor, J. C., Rumble, R. H. and Mee, D. J. (2011). Prediction of noise from small to medium sized crowds. In: David J. Mee and Ian Hillock, Acoustics 2011: Breaking New Ground: Proceedings of the Annual Conference of the Australian Acoustical Society. Acoustics 2011: Breaking New Ground, Gold Coast, Australia, (1-7). 2-4 November 2011.

  • Chan, W. Y. K., Mee, D. J., Smart, M. K., Turner, J. C. and Stalker, R. J. (2010). Boundary layer combustion for viscous drag reduction in practical scramjet configurations. In: I. Grant, 27th International Congress of The Aeronautical Sciences (ICAS 2010), Nice, France, (1-10). 19-24 September 2010.

  • Michael Creagh and Mee, David J. (2009). Attitude guidance for spinning vehicles with independent pitch and yaw control. In: 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 47th AIAA Aerospace Sciences Meeting, Orlando , Florida, USA, (1-16). 5-8 January 2009.

  • Mee, David J., Stalker, Raymond J., Suraweera, Milinda V., Tanimizu, Katsuyoshi, Kirchhartz, Rainer M., Ridings, Andrew N. and Chan, Wilson Y. K. (2008). Force measurements and drag reduction. In: Proceedings of the Australian Hypersonics Capabilities and Future Directions Workshop 2008. Australian Hypersonics Capabilities and Future Directions Workshop 2008, Brisbane, Australia, (). 14-15 August 2008.

  • Kirchhartz, Rainer M., Mee, David J. and Stalker, Raymond J. (2008). Skin Friction Drag with Boundary Layer Combustion in a Circular Combustor. In: 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, United States, (1-10). 28 April - 1 May 2008.

  • Tanimizu, K., Mee, D. J. and Stalker, R. J. (2007). Comparison of drag measurements of two axisymmetric scramjet models at Mach 6. In: Peter Jacobs, Tim McIntyre, Matthew Cleary, David Buttsworth, David Mee, Rose Clements, Richard Morgan and Charles Lemckert, 16th Australasian Fluid Mechanics Conference (AFMC). 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, (1299-1303). 3-7 December, 2007.

  • Kirchhartz, R. M., Mee, D. J. and Stalker, R. J. (2007). Effect of Boundary Layer Thickness and Entropy Layer on Boundary Layer Combustion. In: Peter Jacobs, Tim McIntyre, Matthew Cleary, David Buttsworth, David Mee, Rose Clements, Richard Morgan and Lemckert, C., Proceedings of Sixteenth Australasian Fluid Mechanics Conference. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, (491-496). 3-7 December, 2007.

  • Gangurde, Dhananjay Y., Mee, David J. and Jacobs, Peter A. (2007). Numerical Simulation of a Ludwieg-tube Fuel Delivery System for Scramjet Experiments in Shock Tunnels. In: Peter Jacobs, Tim McIntyre, Matthew Cleary, David Buttsworth, David Mee, Rose Clements, Richard Morgan and Charles Lemckert, 16th Australasian Fluid Mechanics Conference (AFMC). 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, (645-649). 2-7 December 2007.

  • Mee, David J. (2007). Supersonic combustion experiments in the T4 Shock Tunnel. In: R. K. Shama, V. Ramanujachari, U. Raju Babu, R. Gopalaswami and J. D. A. Subramaniam, Challenges in High Speed Transatmospheric Air and Space Transportation: Proceedings of the First International Conference on High Speed Transatmospheric Air and Space Transportation. First International Conference on High Speed Transatmospheric Air and Space Transportation, Hyderabad, India, (288-294). 29-30 June 2007.

  • Tanimizu, K, Mee, D J and Stalker, R J (2006). Measurement and prediction of the force of an unfuelled axisymmetric scramjet model. In: 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, (1-9). 6-9 November 2006.

  • Ramanah, D and Mee, D J (2006). Scramjet flow visualization using background oriented schlieren in hypersonic impulse facilities. In: 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, (1-10). 6-9 November 2006.

  • Raghunath, S., Mee, D., Roesgen, T. and Jacobs, P. (2005). Background oriented schlieren technique for flow visualisation in shock tunnels. In: G. Jagadeesh, E. Arunan and K. Reddy, Shock Waves: Proceedings of the 25th International Symposium on Shock Waves. 25th International Symposium on Shock Waves- ISSW25, Bangalore, India, (). 17-22 July 2005.

  • Denman, Andrew W., Jacobs, Peter A. and Mee, David J. (2005). Compressible, turbulent flow with boundary-layer heat addition. In: AIAA journal: 43rd AIAA Aerospace Sciences Meeting and Exhibit. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, (1-10). 10 - 13 Jan 2005.

  • Hayne, MJ, Mee, DJ, Gai, SL, Stewart, BS and Morgan, RG (2005). Flow establishment over rearward-facing steps in high enthalpy flows. In: Shock Waves, Vols 1 and 2, Proceedings. 24th International Symposium on Shock Waves, Beijing Peoples R China, (173-178). Jul 11-16, 2004. doi:10.1007/978-3-540-27009-6_23

  • Hayne, Michael J., Mee, David J. and Rumble, Ron (2005). Influence of music genre and composition on entertainment noise limits. In: McMinn, Terrance, Proceedings of: Acoustics 2005: acoustics in a changing environment. Acoustics 2005: Acoustics in a Changing Environment, Busselton, Western Australia, (217-224). 9-11 November, 2005.

  • Hayne, M. J., Gai, S. L., Mee, D. J. and Morgan, R. G. (2005). Real gas effects on flows over rearward-facing steps in high enthalpy flows. In: Zonglin Jiang, Shock Waves: Proceedings of the 24th International Symposium on Shock Waves. 24th International Symposium on Shock Waves, Beijing, China, (251-256). 11-16 July 2004. doi:10.1007/978-3-540-27009-6_36

  • Suraweera, Milinda, Mee, David J. and Stalker, Raymond J. (2005). Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, (). 10-13 January, 2005.

  • Hayne, M. J., Mee, D. J., Gai, S. L., Stewart, B. S. and Morgan, R. G. (2004). Flow establishment over rearward-facing steps in high enthalpy flows. In: Zonglin Jiang, Shock Waves: Proceedings of the 24th International Symposium on Shock Waves. 24th International Symposium on Shock Waves, Beijing, China, (). 11-16 July 2004.

  • Raghunath, S., Mee, D. J., Roesgen, T. and Jacobs, P. A. (2004). Flow visualization in the Drummond shock tunnel using the background oriented schlieren technique. In: 9th International Workshop on Shock Tube Technology, Woomera, South Australia, (). 27 September- 1 October 2004.

  • Robinson, Matthew J. and Mee, David J. (2004). Performance measurements in a shock tunnel of a fuelled scramjet vehicle generating lift, thrust and pitching moment. In: Zonglin Jiang, Shock Waves: Proceedings of the 24th International Symposium on Shock Waves. 24th International Symposium on Shock Waves, Beijing, China, (). 11-16 July 2004.

  • Trenker, M., Mee, D. J. and Stalker, R. J. (2004). Reducing skin friction by boundary layer combustion on a generic scramjet model. In: Zonglin Jiang, Shock Waves: Proceedings of the 24th International Symposium on Shock Waves. 24th International Symposium on Shock Waves, Beijing, China, (903-908). 11-16 July 2004.

  • Mee, D. J., Jacobs, P. A., Reddy, K. P. J., Rajakumar, B. and Arunan, E. (2004). Simulation of the performance of a shock tube for studying chemical kinetics. In: 9th International Workshop on Shock Tube Technology, Woomera, Australia, (). 27 September - 1 October 2004.

  • Raghunath, Sreekanth, Mee, David J., Roesgen, Thomas and Jacobs, Peter A. (2004). Visualization Of Supersonic Flows In Shock Tunnels, Using The Background Oriented Schlieren Technique. In: 2004 AIAA Australian Aerospace Student Conference, The University of Sydney, Sydney, (). 12 December, 2004.

  • Robinson, M. J., Mee, D. J. and Paull, A. (2003). Measurement of the aerodynamic performance of a scramjet-powered vehicle in a shock tunnel. In: David J. Mee, Proceedings of the 10th Australian International Aerospace Congress and 14th National Space Engineering Symposium 2003. Century of Aerospace Brisbane 2003, Brisbane, Queensland, Australia, (). 29 July - 1 August 2003.

  • Jokic, M. D., Daniel, W. J. T., Asokanthan, S. F. and Mee, D. J. (2002). Aeroassisted maneuvering of elastic tethered systems using a dissipative time-stepping algorithm. In: 40th AIAA Aerospace Sciences Meeting. 40th AIAA Aerospace Sciences Meeting, Reno, Nevada, USA, (1-10). 14-17 January, 2002.

  • Mee, D. J., Weiland, M.K.H. and Paull, A. (2002). Drag on a slender cone at mach 6.6 with film ejection of hydrogen. In: Proceedings of the Twenty-Third International Symposium on Shock Waves. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, (565-571). 23-27 July, 2001.

  • Hayne, M. J., Gai, S.L., Hillier, R., Morgan, R. G., Mee, D. J. and Mcintyre, T. J. (2002). Heat transfer and flow behind a rearward facing step in a super-orbital expansion tube. In: Proceedings of the Twenty-Third International Symposium on Shock Waves. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, (565-571). 23-27 July, 2001.

  • Robinson, M. J., Mee, D. J. and Paull, A. (2002). Lift, pitching moment and thrust measurement on a fuelled scramjet. In: Proceedings of the Twenty-Third International Symposium on Shock Waves. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, (565-571). 23-27 July, 2001.

  • Abdel-Jawad, M., Morgan, R. G. and Mee, D. J. (2002). Sonic jump for planetary entry vehicles. In: 11th AIAA/AAAF International Conference Space Planes and Hypersonic Systems and Technologies, Orleans, France, (1-19). 29/09/02-04/10/02.

  • Morgan, R. G., Abdel-Jawad, M. and Mee, D. J. (2002). Sonic line location in reacting flows. In: 40th AIAA Aerospace Sciences Meeting. 40th AIAA Aerospace Sciences Meeting, Reno, Nevada, USA, (1-12). 14-17 January, 2002.

  • Abdel-Jawad, M., Mee, D. J., Morgan, R. G. and Chiu, S.H. (2002). Stability tests in superorbital expansion tubes. In: 11th AIAA/AAAF International Conference Space Planes and Hypersonic Systems and Technologies, Orleans, France, (1-10). 29/09/02 - 04/10/02.

  • Abdel-Jawad, M., Mee, D. J., Morgan, R. G., Jacobs, P.A. and Philpot, J.A. (2002). Transient force measurements at superorbital speeds. In: Proceedings of the Twenty-Third International Symposium on Shock Waves. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, (565-571). 23-27 July, 2001.

  • Aminossadati, S. M. and Mee, D. J. (2002). Uncertainty analysis for the measurements of aerodynamic loss of cooled turbine blades. In: P. Pemberton, M. Turner and I. Jacobs, The Fifth Biennial Engineering Mathematics and Applications Conference. The Fifth Biennial Engineering Mathematics and Applications Conference, Queensland University of Technology, Brisbane, (67-72). 29/09/02 - 02/10/02.

  • Macrossan, Michael N., Chiu, H.- H. and Mee, David J. (2001). A test facility for hypervelocity rarefied flows. In: Timothy J. Bartel and Michael A. Gallis, 22nd International Symposium on Rarefied Gas Dynamics (AIP Conference Proceedings), Sydney, Australia, (772-779). 9-14 July, 2000.

  • Jokic, M. D., Asokanthan, S. F., Daniel, W. J. T. and Mee, D. J. (2001). Aerogravity assist manoeuvring of a tethered satellite system. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit. AIAA Atmospheric Flight Mechanics Conference and Exhibit, Montreal, Canada, (1-10). 6-9 August, 2001.

  • Mee, D. J. (2001). Boundary layer transition measurements in hypervelocity flows in a shock tunnel. In: 39th AIAA Aerospace Sciences Meeting and Exhibit. 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, (1-11). 8-11 January, 2001.

  • Gai, S.L., Hayne, M. J., Gardner, A., Morgan, R. G. and Mee, D. J. (2001). Heat transfer behind a step in high enthalpy super-orbital flow. In: 39th AIAA Aerospace Sciences Meeting and Exhibit. 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, (1-8). 8-11 January, 2001.

  • Mee, D. J. (2000). Heat transfer measurements in a transitional boundary layer on a flat plate in a hypervelocity flow. In: Proceedings of the 7th International Workshop on Shock Tube Technology. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, (). 18-20 September, 2000.

  • Frost, M., Paull, A., Alesi, H. and Mee, D. J. (2000). Hyshot scramjet testing in the T4 shock tunnel. In: Proceedings of the 7th International Workshop on Shock Tube Technology. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, (). 18-20 September, 2000.

  • Robinson, M. J., Mee, D. J. and Paull, A. (2000). Simultaneous lift, moment and thrust measurement in hypervelocity flow. In: Proceedings of the 7th International Workshop on Shock Tube Technology. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, (). 18-20 September, 2000.

  • Ishikawa, H. and Mee, D. J. (1999). Numerical investigations of thermoacoustic effects on isothermal plates. In: 61st Meeting on Cryogenics and Superconductivity 1999. 61st Meeting on Cryogenics and Superconductivity, Tokyo, (235-235). 10-12 November 1999.

  • Wendt M., Macrossan M., Jacobs P. and Mee D. (1998). Pilot study for a rarefied hypervelocity test facility. In: Proceedings of the 1998 Thirteenth Australasian Fluid Mechanics Conference, , (59-62). December 13, 1998-December 18, 1998.

  • Morgan R.G., Mee D.J. and Macrossan M.N. (1997). Mechanical and Space Engineering, a degree for undergraduates. In: 35th Aerospace Sciences Meeting and Exhibit. 35th Aerospace Sciences Meeting and Exhibit, 1997, , (). January 6, 1997-January 9, 1997.

  • Aminossadati, S.M. and Mee, D.J. (1995). Simulation of Aerodynamic Loss for Trailing-edge coolant ejection in gas turbine blades. In: Twelfth Australasian Fluid Mechanics Conference. 12th Australasian Fluid Mechanics Conference, Sydney , Australia, (73-76). 10-15 December 1995.

  • Aminossadat, S.M. and Mee, D.J. (1995). Simulation of aerodynamic loss for trailing-edge coolant ejection in gas turbine blades. In: Proceedings of the 12th Australasian Fluid Mechanics Conference. The 12th Australasian Fluid Mechanics Conference, Sydney, NSW, Australia, (73-76). 10-15 December 1995.

  • Tuttle, S. L., Mee, D. J. and Simmons, J. M. (1994). Lift, Drag and Thrust Measurement in a Hypersonic Impulse Facility. In: Proceedings of the AIAA 18th Aerospace Ground Testing Conference. AIAA 18th Aerospace Ground Testing Conference, Colorado Springs, CO, (). 20-23 June, 1994.

  • Stalker, R. J., Simmons, J. M., Paull, A. and Mee, D. J. (1994). Measurement of Scramjet Thrust in Shock Tunnels. In: AIAA 18th Aerospace Ground Testing Conference, Colorado Springs, Colorado, USA, (). 20-23 June, 1994.

  • Paull, A., Stalker, R. J. and Mee, D. J. (1993). Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility. In: AIAA and DGLR, 5th International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, (). 30 November - 3 December, 1993.

  • Mee, D. J., Walton, T. W., Harrison, S. B. and Jones, T. V. (1991). A Comparison of Liquid Crystal Techniques for Transition Detection. In: AIAA 29th Aerospace Sciences Meeting, Reno, Nevada, (). 7-10 January, 1991.

  • Mee, David J. and Stalker, R. J. (1987). Investigation of Weak Shock-Shock and Shock-Expansion Intersection in the Presence of a Turbulent Boundary Layer. In: AIAA 25th Aerospace Sciences Meeting, Reno, Nevada, (). 12-15 January, 1987.

Edited Outputs

Other Outputs

Grants (Administered at UQ)

PhD and MPhil Supervision

Current Supervision

  • Doctor Philosophy — Principal Advisor

    Other advisors:

  • Doctor Philosophy — Principal Advisor

  • Doctor Philosophy — Associate Advisor

    Other advisors:

  • Doctor Philosophy — Associate Advisor

    Other advisors:

  • Doctor Philosophy — Associate Advisor

    Other advisors:

Completed Supervision

Possible Research Projects

Note for students: The possible research projects listed on this page may not be comprehensive or up to date. Always feel free to contact the staff for more information, and also with your own research ideas.