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2015 Conference Publication Turbulent spot initiation rates in boundary layers in a shock tunnelMee, D. J. and Tanguy, G. (2015). Turbulent spot initiation rates in boundary layers in a shock tunnel. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_99 |
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2015 Conference Publication Measurement of three-components of force on an airframe integrated scramjet at Mach 10Doherty, Luke J., Smart, Michael K. and Mee, David J. (2015). Measurement of three-components of force on an airframe integrated scramjet at Mach 10. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3523 |
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2015 Conference Publication Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10Doherty, Luke J., Smart, Michael K. and Mee, David J. (2015). Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, United States, 16– 20 June 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.J053785 |
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2015 Conference Publication Improving sound diffusion in a reverberation chamberMee, David J. and Vallis, Jack (2015). Improving sound diffusion in a reverberation chamber. Acoustics 2015, Hunter Valley, Australia, 15-18 November 2015. NSW Division of the Australian Acoustical Society. |
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2014 Conference Publication Experimental testing of an airframe integrated 3-D scramjet at true mach 10 flight conditionsDoherty, 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. AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014, Atlanta, GA, United States, 16-20 June 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/MHYTASP14 |
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2013 Conference Publication Ethylene augmentation of JP-8+100 in a supersonic combustorBateup, Mark L., Paull, Allan and Mee, David J. (2013). Ethylene augmentation of JP-8+100 in a supersonic combustor. JPC 2013: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, United States, 14-17 July, 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-3700 |
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2012 Conference Publication Design of an airframe integrated 3-D scramjet and experimental results at a Mach 10 flight conditionDoherty, 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. 18th AIAA/3AF International Space Planes and Hypersonics Systems and Technologies Conference, Tours, France, 24 - 28 September 2012. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-5910 |
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2012 Conference Publication Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustionWilson 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. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24-28 September 2012. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-5889 |
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2011 Conference Publication Attitude guidance and control for a spinning, asymmetrical rocket payloadCreagh, Michael A. and Mee, David J. (2011). Attitude guidance and control for a spinning, asymmetrical rocket payload. AIAC14 Fourteenth Australian International Aerospace Congress, Melbourne, Australia, 28 February - 3 March 2011. Melbourne, Australia: Australian International Aerospace Congress. |
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2011 Conference Publication Prediction of noise from small to medium sized crowdsHayne, M. J., Taylor, J. C., Rumble, R. H. and Mee, D. J. (2011). Prediction of noise from small to medium sized crowds. Acoustics 2011: Breaking New Ground, Gold Coast, Australia, 2-4 November 2011. Darlinghurst, Australia: The Australian Acoustical Society. |
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2010 Conference Publication Boundary layer combustion for viscous drag reduction in practical scramjet configurationsChan, 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. 27th International Congress of The Aeronautical Sciences (ICAS 2010), Nice, France, 19-24 September 2010. United Kingdom: Optimage. |
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2009 Conference Publication Attitude guidance for spinning vehicles with independent pitch and yaw controlMichael Creagh and Mee, David J. (2009). Attitude guidance for spinning vehicles with independent pitch and yaw control. 47th AIAA Aerospace Sciences Meeting, Orlando , Florida, USA, 5-8 January 2009. Reston, VA, U.S.: American Institute of Aeronautics and Astronautics. |
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2008 Conference Publication Skin Friction Drag with Boundary Layer Combustion in a Circular CombustorKirchhartz, Rainer M., Mee, David J. and Stalker, Raymond J. (2008). Skin Friction Drag with Boundary Layer Combustion in a Circular Combustor. 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, United States, 28 April - 1 May 2008. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2008-2589 |
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2008 Conference Publication Force measurements and drag reductionMee, 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. Australian Hypersonics Capabilities and Future Directions Workshop 2008, Brisbane, Australia, 14-15 August 2008. |
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2007 Conference Publication Numerical Simulation of a Ludwieg-tube Fuel Delivery System for Scramjet Experiments in Shock TunnelsGangurde, 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. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 2-7 December 2007. Brisbane, Australia: School of Engineering, The University of Queensland. |
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2007 Conference Publication Supersonic combustion experiments in the T4 Shock TunnelMee, David J. (2007). Supersonic combustion experiments in the T4 Shock Tunnel. First International Conference on High Speed Transatmospheric Air and Space Transportation, Hyderabad, India, 29-30 June 2007. Aeronautical Society of India and the Astronautical Society of India. |
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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 |
