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2006 Conference Publication Development of the Hyshot Stability DemonstratorNeuenhahn, T, Olivier, H and Paull, A (2006). Development of the Hyshot Stability Demonstrator. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, California, USA, 5-8 June 2006. USA: American Institute of Aeronautics and Astronautics. |
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2006 Journal Article Performance of a scramjet combustor with combined normal and tangential fuel injectionRowan, S. A. and Paull, A. (2006). Performance of a scramjet combustor with combined normal and tangential fuel injection. Journal Of Propulsion And Power, 22 (6), 1334-1338. doi: 10.2514/1.18744 |
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2006 Journal Article Flight data analysis of the HyShot 2 scramjet flight experimentSmart, M. K., Hass, N. E. and Paull, A. (2006). Flight data analysis of the HyShot 2 scramjet flight experiment. AIAA Journal, 44 (10), 2366-2375. doi: 10.2514/1.20661 |
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2006 Conference Publication Experiments on external combusion with leading edge fuel-injection in hypersonic flowCoras, S. J. and Paull, A (2006). Experiments on external combusion with leading edge fuel-injection in hypersonic flow. 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 Flight data analysis of HyShot 2Mass, Neal E., Smart, Michael K. and Paull, Allan (2005). Flight data analysis of HyShot 2. |
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2005 Conference Publication A 256 channel high speed modular flight computer for hypersonic launch vehiclesFinlayson, Simon and Paull, Allan (2005). A 256 channel high speed modular flight computer for hypersonic launch vehicles. |
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2005 Conference Publication Performance of a scramjet combustor with combined normal and tangential fuel injectionRowan, Scott A. and Paull, Allan (2005). Performance of a scramjet combustor with combined normal and tangential fuel injection. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2005-615 |
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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 Flight Data Analysis of HyShot 2Hass, Neal E., Smart, Michael K. and Paull, Allan (2005). Flight Data Analysis of HyShot 2. 13th AIAA/CIRA International Space Planes and Hypersonic Systems Technologies Conference, Capua, Italy, 16-20 May 2005. Hampton, Virginia, U.S.A.: NASA Langley Research Center. |
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2005 Conference Publication Operating conditions in UQ's impulse facilities for scramjet testingMcGilvray, M., Morgan, R. G., Paull, A., Abdel-Jawad, M. M., Jacobs, P. A., McIntyre, T. J. and Scott, M. A. (2005). Operating conditions in UQ's impulse facilities for scramjet testing. 25th International Symposium on Shock Waves, Bangalore, India, 17-22 July 2005. |
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2004 Conference Publication Ground testing of the hyshot supersonic combustion flight experiment in HEG and comparison with flight dataGardner, A. D., Hannemann, K., Steelant, J. and Paull, A. (2004). Ground testing of the hyshot supersonic combustion flight experiment in HEG and comparison with flight data. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2004-3345 |
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2004 Journal Article Effects of hydrogen-air non-equilibrium chemistry on the performance of a model scramjet thrust nozzleStalker, R. J., Truong, N. K., Morgan, R. G. and Paull, A. (2004). Effects of hydrogen-air non-equilibrium chemistry on the performance of a model scramjet thrust nozzle. Aeronautical Journal, 108 (November), 575-584. doi: 10.1017/S0001924000000403 |
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2004 Conference Publication Investigation of an intake injected hot-wall scramjetKovachevich, A., Paull, A. and McIntyre, Tim J. (2004). Investigation of an intake injected hot-wall scramjet. 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 5-8 January ,2004. doi: 10.2514/6.2004-1037 |
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2003 Conference Publication Comparison of experimental thrust measurements with theoretical values for a scramjet engineOdam, J. and Paull, A. (2003). Comparison of experimental thrust measurements with theoretical values for a scramjet engine. |
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2003 Journal Article Combustor and nozzle CFD calculations for the HyShot Scramjet flight experimentBoyce, R. R., Frost, M. and Paull, A. (2003). Combustor and nozzle CFD calculations for the HyShot Scramjet flight experiment. Computational Fluid Dynamics Journal, 12 (2(28)), 216-226. |
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2003 Conference Publication The HyShot Scramjet Flight Experiment - Flight Data and CFD Calculations ComparedBoyce, Russell R., Gerard, Sullivan and Paull, Allan (2003). The HyShot Scramjet Flight Experiment - Flight Data and CFD Calculations Compared. AIAA 12th International Space Planes and Hypersonics Systems and Technologies Conference, Norfolk, Virginia, 15-19 December 2003. Reston, Va: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2003-7029 |
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2003 Journal Article Skin-friction measurements in high-enthalpy hypersonic boundary layersGoyne, C. P., Stalker, R. J. and Paull, A. (2003). Skin-friction measurements in high-enthalpy hypersonic boundary layers. Journal of Fluid Mechanics, 485 (485), 1-32. doi: 10.1017/S0022112003003975 |
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2003 Conference Publication The Methodology behind the Hyshot Flight ProgramPaull, A., Alesi, H. and Anderson, S. M. (2003). The Methodology behind the Hyshot Flight Program. 10th Australian International Aerospace Congress, Brisbane, Queensland, Australia, 29 July - 1 August 2003. ACT, Australia: Engineers Australia. |
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2003 Conference Publication CFD calculations for intake-injection shock-induced-combustion scramjet flight experimentsMudford, N. R., Mulreany, P. J., McGuire, J. R., Odam, J., Boyce, R. R. and Paull, A. (2003). CFD calculations for intake-injection shock-induced-combustion scramjet flight experiments. AIAA 12th International Space Planes and Hypersonics Systems and Technologies Conference, Norfolk, Virginia, 15-19 December, 2003. Reston, Va: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2003-7034 |
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2003 Conference Publication Measurement of the aerodynamic performance of a scramjet-powered vehicle in a shock tunnelRobinson, M. J., Mee, D. J. and Paull, A. (2003). Measurement of the aerodynamic performance of a scramjet-powered vehicle in a shock tunnel. Century of Aerospace Brisbane 2003, Brisbane, Queensland, Australia, 29 July - 1 August 2003. Barton, A.C.T., Australia: Engineers Australia. |
