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2007 Conference Publication Comparison of drag measurements of two axisymmetric scramjet models at Mach 6Tanimizu, K., Mee, D. J. and Stalker, R. J. (2007). Comparison of drag measurements of two axisymmetric scramjet models at Mach 6. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Australia: School of Engineering, The University of Queensland. |
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2007 Conference Publication Effect of Boundary Layer Thickness and Entropy Layer on Boundary Layer CombustionKirchhartz, R. M., Mee, D. J. and Stalker, R. J. (2007). Effect of Boundary Layer Thickness and Entropy Layer on Boundary Layer Combustion. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Australia: School of Engineering, The University of Queensland. |
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2006 Conference Publication Measurement and prediction of the force of an unfuelled axisymmetric scramjet modelTanimizu, Katsuyoshi, Mee, David J. and Stalker, Raymond J. (2006). Measurement and prediction of the force of an unfuelled axisymmetric scramjet model. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2006-8064 |
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2006 Conference Publication Scramjet flow visualization using Background Oriented Schlieren in hypersonic impulse facilitiesRamanah, Dwishen and Mee, David J. (2006). Scramjet flow visualization using Background Oriented Schlieren in hypersonic impulse facilities. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2006-8004 |
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2006 Conference Publication Prediction of crowd noiseHayne, M. J., Rumble, R. H. and Mee, D. J. (2006). Prediction of crowd noise. 1st Australasian Acoustical Societies' Conference 2006: Noise of Progress, ACOUSTICS 2006, , , November 20, 2006-November 22, 2006. |
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2006 Conference Publication Measurement and prediction of the force of an unfuelled axisymmetric scramjet modelTanimizu, K, Mee, D J and Stalker, R J (2006). Measurement and prediction of the force of an unfuelled axisymmetric scramjet model. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, 6-9 November 2006. USA: American Institute of Aeronautics and Astronautics. |
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2006 Conference Publication Scramjet flow visualization using background oriented schlieren in hypersonic impulse facilitiesRamanah, D and Mee, D J (2006). Scramjet flow visualization using background oriented schlieren in hypersonic impulse facilities. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, 6-9 November 2006. USA: American Institute of Aeronautics and Astronautics. |
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2005 Conference Publication Influence of music genre and composition on entertainment noise limitsHayne, Michael, Mee, David and Rumble, Ron (2005). Influence of music genre and composition on entertainment noise limits. Annual Conference of the Australian Acoustical Society 2005: Acoustics in a Changing Environment, Acoustics 2005, , , November 9, 2005-November 11, 2005. |
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2005 Conference Publication Real gas effects on flows over rearward-facing steps in high enthalpy flowsHayne, 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. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. doi: 10.1007/978-3-540-27009-6_36 |
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2005 Conference Publication Compressible, turbulent flow with boundary-layer heat additionDenman, Andrew W., Jacobs, Peter A. and Mee, David J. (2005). Compressible, turbulent flow with boundary-layer heat addition. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 10 - 13 Jan 2005. Reston, Va.: American Institute of Aeronautics and Astronautics. |
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2005 Conference Publication Background oriented schlieren technique for flow visualisation in shock tunnelsRaghunath, S., Mee, D., Roesgen, T. and Jacobs, P. (2005). Background oriented schlieren technique for flow visualisation in shock tunnels. 25th International Symposium on Shock Waves- ISSW25, Bangalore, India, 17-22 July 2005. India: Universities Press. |
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2005 Conference Publication Influence of music genre and composition on entertainment noise limitsHayne, Michael J., Mee, David J. and Rumble, Ron (2005). Influence of music genre and composition on entertainment noise limits. Acoustics 2005: Acoustics in a Changing Environment, Busselton, Western Australia, 9-11 November, 2005. Castlemaine, VIC, Australia: Australian Acoustical Society. |
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2005 Conference Publication Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer CombustionSuraweera, Milinda, Mee, David J. and Stalker, Raymond J. (2005). Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 10-13 January, 2005. doi: 10.2514/6.2005-613 |
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2005 Conference Publication Flow establishment over rearward-facing steps in high enthalpy flowsHayne, MJ, Mee, DJ, Gai, SL, Stewart, BS and Morgan, RG (2005). Flow establishment over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing Peoples R China, Jul 11-16, 2004. BERLIN: SPRINGER-VERLAG BERLIN. doi: 10.1007/978-3-540-27009-6_23 |
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2004 Conference Publication Visualization Of Supersonic Flows In Shock Tunnels, Using The Background Oriented Schlieren TechniqueRaghunath, Sreekanth, Mee, David J., Roesgen, Thomas and Jacobs, Peter A. (2004). Visualization Of Supersonic Flows In Shock Tunnels, Using The Background Oriented Schlieren Technique. 2004 AIAA Australian Aerospace Student Conference, The University of Sydney, Sydney, 12 December, 2004. |
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2004 Conference Publication Reducing skin friction by boundary layer combustion on a generic scramjet modelTrenker, M., Mee, D. J. and Stalker, R. J. (2004). Reducing skin friction by boundary layer combustion on a generic scramjet model. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. doi: 10.1007/978-3-540-27009-6_137 |
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2004 Conference Publication Three-component force measurements on a large scramjet in a shock tunnelRobinson, M. J., Mee, D. J., Tsai, C. Y. and Bakos, R. J. (2004). Three-component force measurements on a large scramjet in a shock tunnel. USA: American Institute of Aeronautics and Astronautics, Inc. doi: 10.2514/1.10699 |
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2004 Conference Publication Performance measurements in a shock tunnel of a fuelled scramjet vehicle generating lift, thrust and pitching momentRobinson, Matthew J. and Mee, David J. (2004). Performance measurements in a shock tunnel of a fuelled scramjet vehicle generating lift, thrust and pitching moment. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. doi: 10.1007/978-3-540-27009-6_134 |
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2004 Conference Publication Flow visualization in the Drummond shock tunnel using the background oriented schlieren techniqueRaghunath, S., Mee, D. J., Roesgen, T. and Jacobs, P. A. (2004). Flow visualization in the Drummond shock tunnel using the background oriented schlieren technique. 9th International Workshop on Shock Tube Technology, Woomera, South Australia, 27 September- 1 October 2004. |
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2004 Conference Publication Simulation of the performance of a shock tube for studying chemical kineticsMee, 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. 9th International Workshop on Shock Tube Technology, Woomera, Australia, 27 September - 1 October 2004. |
