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2002 Journal Article Upstream porthole injection in a 2-D scramjet modelGardner, A. D., Paull, A. and McIntyre, T. J. (2002). Upstream porthole injection in a 2-D scramjet model. Shock Waves, 11 (5), 369-375. doi: 10.1007/s001930200120 |
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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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2002 Journal Article Transducer for direct measurement of skin friction in hypervelocity impulse facilitiesGoyne, C.P., Stalker, R.J. and Paull, A. (2002). Transducer for direct measurement of skin friction in hypervelocity impulse facilities. Aiaa Journal, 40 (1), 42-49. doi: 10.2514/2.1639 |
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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 Journal Article Skin-friction measurements in a supersonic combustor with crossflow fuel injectionTanno, H., Paull, A. and Stalker, R. J. (2001). Skin-friction measurements in a supersonic combustor with crossflow fuel injection. Journal of Propulsion And Power, 17 (6), 1333-1338. doi: 10.2514/2.5883 |
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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 Journal Article Hypervelocity skin-friction reduction by boundary-layer combustion of hydrogenGoyne, CP, Stalker, RJ, Paull, A and Brescianini, CP (2000). Hypervelocity skin-friction reduction by boundary-layer combustion of hydrogen. Journal of Spacecraft and Rockets, 37 (6), 740-746. doi: 10.2514/2.3645 |
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2000 Journal Article Unstarted inlet for direct-connect combustor experiments in a shock tunnelBoyce, R. R., Paull, A. and Stalker, R. J. (2000). Unstarted inlet for direct-connect combustor experiments in a shock tunnel. Journal of Propulsion and Power, 16 (4), 718-720. doi: 10.2514/2.5633 |
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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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2000 Journal Article Comparison of supersonic combustion beetween impulse and vitiation-heated facilitiesBoyce, R., Paull, A., Stalker, R. J., Wendt, M., Chinzei, N. and Miyajima, H. (2000). Comparison of supersonic combustion beetween impulse and vitiation-heated facilities. Journal of Propulsion and Power, 16 (4), 709-717. doi: 10.2514/2.5631 |
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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 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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1999 Journal Article Shock-tunnel skin-friction measurement in a supersonic combustorStalker, RJ and Paull, A (1999). Shock-tunnel skin-friction measurement in a supersonic combustor. Journal of Propulsion and Power, 15 (5), 699-705. doi: 10.2514/2.5481 |
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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. |
