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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 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. |
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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 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 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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2002 Conference Publication Lift, pitching moment and thrust measurement on a fuelled scramjetRobinson, M. J., Mee, D. J. and Paull, A. (2002). Lift, pitching moment and thrust measurement on a fuelled scramjet. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23. |
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2002 Conference Publication Hyshot flight programPaull, A. and Alesi, H. (2002). Hyshot flight program. The Fifth Biennial Engineering Mathematics and Applications Ce, Queensland University of Technology, Brisbane, 29/09/02 - 02/10/02. Brisbane: Queensland University of Technology. |
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2002 Conference Publication Drag on a slender cone at mach 6.6 with film ejection of hydrogenMee, D. J., Weiland, M.K.H. and Paull, A. (2002). Drag on a slender cone at mach 6.6 with film ejection of hydrogen. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23. |
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2002 Conference Publication Combustor and nozzle CFD calculations for the HyShot scramjet flight experimentBoyce, R. R., Frost, M. and Paull, A. (2002). Combustor and nozzle CFD calculations for the HyShot scramjet flight experiment. AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans, France, 29 Sep - 4 Oct 2002. Reston, Virginia: AIAA - American Institute of Aeronautics and Astronautics. |
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2002 Conference Publication In-situ sampling of gases and debris from volcanic plumesTakayama, K., Saito, T., Sasoh, A., Taniguchi, H. and Paull, A. (2002). In-situ sampling of gases and debris from volcanic plumes. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23. |
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2001 Conference Publication Viscous drag reduction in a scramjet combustor with film coolingRowan, S. and Paull, A. (2001). Viscous drag reduction in a scramjet combustor with film cooling. 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, , , April 24, 2001-April 27, 2001. Reston, Virigina: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2001-1818 |
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2001 Conference Publication Scramjet intake and exhaust CFD studies for the HyShot scramjet flight experimentBoyce R.R. and Paull A. (2001). Scramjet intake and exhaust CFD studies for the HyShot scramjet flight experiment. 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, April 24, 2001-April 27, 2001. doi: 10.2514/6.2001-1891 |
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2000 Conference Publication Pressure measurements in a scramjet combustor with film coolingRowan, S. and Paull, A. (2000). Pressure measurements in a scramjet combustor with film cooling. Reston, Virigina: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2000-2443 |
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2000 Conference Publication Hypersonic airbreathing propulsionPaull, A. (2000). Hypersonic airbreathing propulsion. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton. |
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2000 Conference Publication Simultaneous lift, moment and thrust measurement in hypervelocity flowRobinson, M. J., Mee, D. J. and Paull, A. (2000). Simultaneous lift, moment and thrust measurement in hypervelocity flow. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, 18-20 September, 2000. Long Island, New York, USA: GASL. |
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2000 Conference Publication Hyshot scramjet testing in the T4 shock tunnelFrost, M., Paull, A., Alesi, H. and Mee, D. J. (2000). Hyshot scramjet testing in the T4 shock tunnel. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, 18-20 September, 2000. Long Island, New York, USA: GASL. |
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1999 Conference Publication Upstream porthole injection in a 2-D scramjet modelGardner, A., Paull, A. and McIntyre, T. J. (1999). Upstream porthole injection in a 2-D scramjet model. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton. |
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1999 Conference Publication Scram jet measurements in a shock tunnelPaull A. (1999). Scram jet measurements in a shock tunnel. 35th Joint Propulsion Conference and Exhibit, 1999, June 20, 1999-June 24, 1999. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1999-2450 |
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1999 Conference Publication Intake design for a scramjet flight experimentBoyce, R. and Paull, A. (1999). Intake design for a scramjet flight experiment. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton. |
