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2019 Conference Publication Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared ThermographyRamesh, Ranjini, Kelly, Rory, Cullen, Timothy G., Morgan, Richard G. and Mee, David J. (2019). Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared Thermography. AIAA Aviation 2019 Forum, Dallas, TX, United States, 17-21 June 2019. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3006 |
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2019 Conference Publication Magnetohydrodynamic drag force measurements in expansion tubes using an accelerometerSmith, Daniel R., Gildfind, David E. , James, Christopher M., Andrianatos, Andreas, Mee, David J. and McIntyre, Timothy J. (2019). Magnetohydrodynamic drag force measurements in expansion tubes using an accelerometer. 32nd International Symposium on Shock Waves, Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0145-cd |
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2019 Conference Publication Testing and performance quantification of acoustic louvresHayne, Michael, Tan, Dexter, Devereux, Richard and Mee, David (2019). Testing and performance quantification of acoustic louvres. Australian Acoustical Society Annual Conference, AAS 2018, Adelaide, SA Australia, 7-9 November 2018. Toowong, QLD Australia: Australian Acoustical Society. |
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2019 Conference Publication Stress wave force balance sting design for magnetohydrodynamic drag force measurements in expansion tubesSmith, Daniel R., Gildfind, David E., McIntyre, Timothy J. and Mee, David J. (2019). Stress wave force balance sting design for magnetohydrodynamic drag force measurements in expansion tubes. Asia Pacific International Symposium on Aerospace Technology (APISAT 2019), Gold Coast, QLD, Australia, 4-6 December 2019. |
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2019 Conference Publication Removal of continuous extraneous noise from exceedance levelsHugall, B., Brown, R. and Mee, D. J. (2019). Removal of continuous extraneous noise from exceedance levels. Australian Acoustical Society Annual Conference, AAS 2018, Adelaide, SA Australia, 7-9 November 2018. Toowong, QLD Australia: Australian Acoustical Society. |
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2017 Journal Article Estimating turbulent spot initiation rates from transition lengths in hypersonic boundary layersRaghunath, Sreekanth, Mee, David and Narasimha, Roddam (2017). Estimating turbulent spot initiation rates from transition lengths in hypersonic boundary layers. AIAA Journal, 55 (11), 3640-3647. doi: 10.2514/1.J055502 |
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2017 Conference Publication Dependence of turbulent Sspot initiation rates on hypersonic boundary layer flow parametersRaghunath, Sreekanth , Narasimha, Roddam and Mee, David J. (2017). Dependence of turbulent Sspot initiation rates on hypersonic boundary layer flow parameters. 55th AIAA Aerospace Sciences Meeting and Exhibit, Dallas, TX, United States, 9-13 January 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-1684 |
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2016 Conference Publication Boundary layer transition in hypersonic flowsMee, D. J. and Raghunath, S. (2016). Boundary layer transition in hypersonic flows. Franco-Australian Symposium on Hypersonics and High Enthalpy Flows, Châtenay-Malabry, France, 7-9 September 2016. |
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2016 Conference Publication Force Measurement in Impulse Hypersonic FacilitiesMee, D. J. (2016). Force Measurement in Impulse Hypersonic Facilities. First International Symposium on Hypersonics, Korean Advanced Institute of Science and Technology, 27-30 November 2016. |
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2016 Book Chapter Free piston shock tunnels HEG, HIEST, T4 and T5Hannemann, Klaus, Itoh, Katsuhiro, Mee, David J. and Hornung, Hans G. (2016). Free piston shock tunnels HEG, HIEST, T4 and T5. Experimental methods of shock wave research. (pp. 181-264) edited by Hans Grönig, Yasuyuki Horie and Kazuyoshi Takayama. London, United Kingdom: Springer International Publishing. doi: 10.1007/978-3-319-23745-9_7 |
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2016 Conference Publication UQ research in transitional flowsMee, D. J. and Raghunath, S. (2016). UQ research in transitional flows. 1st French-Australian Workshop on Re-entry and Hypersonic Aerothermodynamics, Brisbane, QLD, Australia, 23-25 February, 2016. |
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2016 Conference Publication Performance Comparison of Distributed Injection Methods for Hypersonic Film-CoolingBasore, 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. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, 5-8 December 2016. Victoria, Australia: Australasian Fluid Mechanics Society. |
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2015 Journal Article Drag reduction by boundary-layer combustion: influence from disturbances typical of cross-stream fuel-injectionChan, Wilson Y. K., Mee, David J., Smart, Michael K. and Turner, James C. (2015). Drag reduction by boundary-layer combustion: influence from disturbances typical of cross-stream fuel-injection. Journal of Propulsion and Power, 31 (5), 1486-1491. doi: 10.2514/1.B35665 |
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2015 Journal Article Drag reduction by boundary-layer combustion: effects of flow disturbances from rectangular-to-elliptical-shape-transition inletsChan, Wilson Y. K., Mee, David J., Smart, Michael K. and Turner, James C. (2015). Drag reduction by boundary-layer combustion: effects of flow disturbances from rectangular-to-elliptical-shape-transition inlets. Journal of Propulsion and Power, 31 (5), 1256-1267. doi: 10.2514/1.B35335 |
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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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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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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 Journal Article Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditionsTanimizu, Katsuyoshi, Mee, David J., Stalker, Raymond J. and Jacobs, Peter A. (2013). Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions. Shock Waves, 23 (5), 453-460. doi: 10.1007/s00193-013-0449-4 |
