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2016

Conference Publication

Force Measurement in Impulse Hypersonic Facilities

Mee, 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.

Force Measurement in Impulse Hypersonic Facilities

2016

Book Chapter

Free piston shock tunnels HEG, HIEST, T4 and T5

Hannemann, 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

Free piston shock tunnels HEG, HIEST, T4 and T5

2015

Journal Article

Drag reduction by boundary-layer combustion: effects of flow disturbances from rectangular-to-elliptical-shape-transition inlets

Chan, 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

Drag reduction by boundary-layer combustion: effects of flow disturbances from rectangular-to-elliptical-shape-transition inlets

2015

Journal Article

Drag reduction by boundary-layer combustion: influence from disturbances typical of cross-stream fuel-injection

Chan, 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

Drag reduction by boundary-layer combustion: influence from disturbances typical of cross-stream fuel-injection

2015

Conference Publication

Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10

Doherty, 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

Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10

2015

Conference Publication

Improving sound diffusion in a reverberation chamber

Mee, 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.

Improving sound diffusion in a reverberation chamber

2015

Conference Publication

Turbulent spot initiation rates in boundary layers in a shock tunnel

Mee, 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

Turbulent spot initiation rates in boundary layers in a shock tunnel

2015

Conference Publication

Measurement of three-components of force on an airframe integrated scramjet at Mach 10

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. 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

Measurement of three-components of force on an airframe integrated scramjet at Mach 10

2014

Conference Publication

Experimental testing of an airframe integrated 3-D scramjet at true mach 10 flight conditions

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. 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

Experimental testing of an airframe integrated 3-D scramjet at true mach 10 flight conditions

2013

Journal Article

Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions

Tanimizu, 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

Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions

2013

Journal Article

An experimental study on aerodynamic performance of turbine nozzle guide vanes with trailing-edge span-wise ejection

Aminossadati, S. M. and Mee, D. J. (2013). An experimental study on aerodynamic performance of turbine nozzle guide vanes with trailing-edge span-wise ejection. Journal of Turbomachinery, 135 (3) 031002, 031002.1-031002.12. doi: 10.1115/1.4006663

An experimental study on aerodynamic performance of turbine nozzle guide vanes with trailing-edge span-wise ejection

2013

Conference Publication

Ethylene augmentation of JP-8+100 in a supersonic combustor

Bateup, 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

Ethylene augmentation of JP-8+100 in a supersonic combustor

2012

Journal Article

Suitability of the k-omega turbulence model for scramjet flowfield simulations

Chan, W. Y. K., Jacobs, P. A. and Mee, D. J. (2012). Suitability of the k-omega turbulence model for scramjet flowfield simulations. International Journal for Numerical Methods in Fluids, 70 (4), 493-514. doi: 10.1002/fld.2699

Suitability of the k-omega turbulence model for scramjet flowfield simulations

2012

Journal Article

Nanoparticle-induced morphology and hydrophilicity of structured surfaces

Gao, Nan, Yan, Yuying, Chen, Xinyong and Mee, David J. (2012). Nanoparticle-induced morphology and hydrophilicity of structured surfaces. Langmuir, 28 (33), 12256-12265. doi: 10.1021/la302627n

Nanoparticle-induced morphology and hydrophilicity of structured surfaces

2012

Journal Article

Supersonic skin-friction drag with tangential wall slot fuel injection and combustion

Kirchhartz, Rainer M., Mee, David J. and Stalker, Raymond J. (2012). Supersonic skin-friction drag with tangential wall slot fuel injection and combustion. AIAA Journal, 50 (2), 313-324. doi: 10.2514/1.J051073

Supersonic skin-friction drag with tangential wall slot fuel injection and combustion

2012

Conference Publication

Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion

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. 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

Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion

2012

Conference Publication

Design of an airframe integrated 3-D scramjet and experimental results at a Mach 10 flight condition

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. 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

Design of an airframe integrated 3-D scramjet and experimental results at a Mach 10 flight condition

2011

Journal Article

Numerical modelling of the self-heating process of a wet porous medium

Ejlali, A., Mee, D.J., Hooman, K. and Beamish, B.B. (2011). Numerical modelling of the self-heating process of a wet porous medium. International Journal of Heat and Mass Transfer, 54 (25-26), 5200-5206. doi: 10.1016/j.ijheatmasstransfer.2011.08.025

Numerical modelling of the self-heating process of a wet porous medium

2011

Journal Article

Superhydrophobic surfaces with hierarchical structure

Gao, N., Yan, Y. Y., Chen, X. Y. and Mee, D. J. (2011). Superhydrophobic surfaces with hierarchical structure. Materials Letters, 65 (19-20), 2902-2905. doi: 10.1016/j.matlet.2011.06.088

Superhydrophobic surfaces with hierarchical structure

2011

Conference Publication

Attitude guidance and control for a spinning, asymmetrical rocket payload

Creagh, 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.

Attitude guidance and control for a spinning, asymmetrical rocket payload