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Frost, Myles A., Gangurde, Dhananjay Y., Paull, Allan and Mee, David J. (2009) Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow. AIAA Journal, 47 4: 1050-1053. doi:10.2514/1.40868 97   2 Cited 4 times in Scopus4 0
Mudford, 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. In: Proceedings of the AIAA 12th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 12th International Space Planes and Hypersonics Systems and Technologies Conference, Norfolk, Virginia, (xx-xx). 15-19 December, 2003. 164  
Boyce, R. R., Frost, M. and Paull, A. (2002). Combustor and nozzle CFD calculations for the HyShot scramjet flight experiment. In: AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans, France, (). 29 Sep - 4 Oct 2002. 141  
Boyce, 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. 100  
Boyce, 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 91   15 0
Ho, S. Y. and Paull, A. (2006) Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test. Aerospace Science And Technology, 10 5: 420-426. doi:10.1016/j.ast.2006.03.004 108   2 Cited 11 times in Scopus11 0
Neuenhahn, T, Olivier, H and Paull, A (2006). Development of the Hyshot Stability Demonstrator. In: 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, California, USA, (1-17). 5-8 June 2006. 74  
Mee, D. J., Weiland, M.K.H. and Paull, A. (2002). Drag on a slender cone at mach 6.6 with film ejection of hydrogen. In: Proceedings of the Twenty-Third International Symposium on Shock Waves. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, (565-571). 23-27 July, 2001. 41  
Stalker, 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. 140   2 Cited 3 times in Scopus3
Bateup, Mark L., Paull, Allan and Mee, David J. (2013). Ethylene augmentation of JP-8+100 in a supersonic combustor. In: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2013: Proceedings. JPC 2013: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, United States, (1164-1173). 14-17 July, 2013. doi:10.2514/6.2013-3700 66 6 Cited 0 times in Scopus0 0
Coras, S. J. and Paull, A (2006). Experiments on external combusion with leading edge fuel-injection in hypersonic flow. In: 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, (1-7). 6-9 November 2006. 78  
Hass, Neal E., Smart, Michael K. and Paull, Allan (2005). Flight Data Analysis of HyShot 2. In: Proceedings of the 13th AIAA/CIRA International Space Planes and Hypersonic Systems Technologies Conference. 13th AIAA/CIRA International Space Planes and Hypersonic Systems Technologies Conference, Capua, Italy, (2005-3354-1-2005-3354-17). 16-20 May 2005. 73  
Smart, 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 264   33 Cited 97 times in Scopus97 0
Paull, A. (2000). Hypersonic airbreathing propulsion. In: G. J. Ball, R. Hillier and G. T. Roberts, Proceedings of the 22nd International Symposium on Shock Waves. 22nd International Symposium on Shock Waves, Imperial College, London, UK, (5-12). 18-23 July, 1999. 68  
Morgan, Richard, Paull, Allan, Smart, Michael and Stalker, Ray (2007). Hypersonics Research in Australia. In: Advances on Propulsion Technology for High-Speed Aircraft: Papers presented during the AVT-150 RTO AVT/VKI Lecture Series. AVT-150 RTO AVT/VKI Lecture Series: Advances on Propulsion Technology for High-Speed Aircraft, Von Karmen Institute for Fluid Mechanics, Rhode St. Genese, Belgium, (11-1-11-30). 12-15 March 2007. 121  
Goyne, 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 115   9 Cited 24 times in Scopus24 0
Paull, A. and Alesi, H. (2002). Hyshot flight program. In: Pemberton, M. Turner, I. Jacobs, P. and ., The Fifth Biennial Engineering Mathematics and Applications Conference. The Fifth Biennial Engineering Mathematics and Applications Ce, Queensland University of Technology, Brisbane, (27-31). 29/09/02 - 02/10/02. 103  
Frost, M., Paull, A., Alesi, H. and Mee, D. J. (2000). Hyshot scramjet testing in the T4 shock tunnel. In: Proceedings of the 7th International Workshop on Shock Tube Technology. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, (). 18-20 September, 2000. 70  
Kovachevich, Anne L., Hajek, Kim M., McIntyre, Timothy J., Paull, Allan and Abdel-Jawad, Madhat (2006). Imaging of hydrogen fuel injection on the intake of a heated wall scramjet. In: 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Proceedings (2006). 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Sacramento, California, (). 9 - 12 July 2006. 100  
Takayama, K., Saito, T., Sasoh, A., Taniguchi, H. and Paull, A. (2002). In-situ sampling of gases and debris from volcanic plumes. In: Proceedings of the Twenty-Third International Symposium on Shock Waves. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, (565-571). 23-27 July, 2001. 38  
Boyce, R. and Paull, A. (1999). Intake design for a scramjet flight experiment. In: G. J. Ball, R. Hillier and G. T. Roberts, Proceedings of the 22nd International Symposium on Shock Waves. 22nd International Symposium on Shock Waves, Imperial College, London, UK, (1477-1482). 18-23 July, 1999. 64  
Hunt, D. C., Paull, A., Boyce, R. R. and Hagenmaier, M. (2009). Investigation of an axisymmetric scramjet configuration utilising inlet-injection and radical farming. In: Hany Moustapha, Proceedings of the 19th International Symposium on. 19th International Symposium on Airbreathing Engines (ISABE2009), Montreal, Canada, (1353-1-1353-10). 7-11 September, 2009. 216  
Kovachevich, A., Paull, A. and McIntyre, Tim J. (2004). Investigation of an intake injected hot-wall scramjet. In: 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, (). 5-8 January ,2004. 75  
Robinson, M. J., Mee, D. J. and Paull, A. (2002). Lift, pitching moment and thrust measurement on a fuelled scramjet. In: Proceedings of the Twenty-Third International Symposium on Shock Waves. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, (565-571). 23-27 July, 2001. 63  
Stalker, R. J., Simmons, J. M., Paull, A. and Mee, D. J. (1994). Measurement of Scramjet Thrust in Shock Tunnels. In: AIAA 18th Aerospace Ground Testing Conference, Colorado Springs, Colorado, USA, (). 20-23 June, 1994. 387 251
Robinson, M. J., Mee, D. J. and Paull, A. (2003). Measurement of the aerodynamic performance of a scramjet-powered vehicle in a shock tunnel. In: David J. Mee, Proceedings of the 10th Australian International Aerospace Congress and 14th National Space Engineering Symposium 2003. Century of Aerospace Brisbane 2003, Brisbane, Queensland, Australia, (). 29 July - 1 August 2003. 70  
Gauer, M. and Paull, Allan (2008) Numerical investigation of a spiked blunt nose cone at hypersonic speeds. Journal of Spacecraft and Rockets, 45 3: 459-471. doi:10.2514/1.30590 154   13 Cited 20 times in Scopus20 0
McGilvray, 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. In: 25th International Symposium on Shock Waves, Bangalore, India, (). 17-22 July 2005. 54  
Rowan, 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 90   5 Cited 9 times in Scopus9 0
Sabean, JW, Lewis, MJ, Mee, D and Paull, A (1999) Performance study of a power law starbody. Journal of Spacecraft and Rockets, 36 5: 646-652. doi:10.2514/2.3496 43   7 0
Robinson, M. J., Mee, D. J. and Paull, A. (2006) Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnel. Journal Of Propulsion And Power, 22 1: 85-95. doi:10.2514/1.15978 115   5 Cited 10 times in Scopus10 0
Stalker, 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.2005.08.002 481 1528 17 Cited 46 times in Scopus46 0
Kirchhartz, Rainer M., Paull, Allan, Mee, David J. and Olivier, Herbert (2010) Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flows. International Journal of Hypersonics, 1 4: 199-208. doi:10.1260/1759-3107.1.4.199 46   0
Stalker, 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 62   8 Cited 18 times in Scopus18 0
Robinson, M. J., Mee, D. J. and Paull, A. (2000). Simultaneous lift, moment and thrust measurement in hypervelocity flow. In: Proceedings of the 7th International Workshop on Shock Tube Technology. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, (). 18-20 September, 2000. 43  
Tanno, 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 53   6 Cited 12 times in Scopus12 0
Goyne, C. P., Stalker, R. J. and Paull, A. (2003) Skin-friction measurements in high-enthalpy hypersonic boundary layers. Journal of Fluid Mechanics, 485 1-32. doi:10.1017/S0022112003003975 108   8 Cited 14 times in Scopus14 0
Boyce, Russell R., Gerard, Sullivan and Paull, Allan (2003). The HyShot Scramjet Flight Experiment - Flight Data and CFD Calculations Compared. In: Proceedings of the AIAA 12th International Space Planes and Hypersonics Systems and Technologies Conference. AIAA 12th International Space Planes and Hypersonics Systems and Technologies Conference, Norfolk, Virginia, (). 15-19 December 2003. 230  
Paull, A., Alesi, H. and Anderson, S. M. (2003). The Methodology behind the Hyshot Flight Program. In: David J. Mee, Proceedings of the 10th Australian International Aerospace Congress, Brisbane, July, 2003 ; and 14th National Space Engineering Symposium 2003. 10th Australian International Aerospace Congress, Brisbane, Queensland, Australia, (). 29 July - 1 August 2003. 47  
Paull, A., Stalker, R. J. and Mee, D. J. (1993). Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility. In: AIAA and DGLR, 5th International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, (). 30 November - 3 December, 1993. 299 222
Goyne, 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 82 552 8 0
Boyce, 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 77   1 0
Gardner, A., Paull, A. and McIntyre, T. J. (1999). Upstream porthole injection in a 2-D scramjet model. In: G. J. Ball, R. Hillier and G. T. Roberts, Proceedings of the 22nd International Symposium on Shock Waves. 22nd International Symposium on Shock Waves, Imperial College, London, UK, (1495-1500). 18-23 July, 1999. 35  
Gardner, 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 83   8 Cited 29 times in Scopus29 0