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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 |
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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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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 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 |
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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 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 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 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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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 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 |
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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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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 Edited Outputs Acoustics 2004 - Transportation Noise and Vibration - the New MillenniumD. J. Mee, R. J. Hooker and I. D. M. Hillock eds. (2004). Acoustics 2004 - Transportation Noise and Vibration - the New Millennium. Proceedings of the annual conference of the Australian Acoustical Society, Gold Coast, Australia, 3-5 November 2004. Australia: Australian Acoustical Society. |
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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 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 Flow establishment over rearward-facing steps in high enthalpy flowsHayne, 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. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. |
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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 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 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 |
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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. |
