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2024 Journal Article STAJe−: A supersonic flight program STAJe− 1 payload design and system studyKunze, Jens, Vijay Shelar, Sampada and Paull, Allan (2024). STAJe−: A supersonic flight program STAJe− 1 payload design and system study. Journal of Spacecraft and Rockets, 61 (1), 233-247. doi: 10.2514/1.a35544 |
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2023 Journal Article Preliminary analysis of the performance of an electric supersonic propellerKunze, Jens and Paull, Allan (2023). Preliminary analysis of the performance of an electric supersonic propeller. Aerospace, 10 (9) 803, 803. doi: 10.3390/aerospace10090803 |
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2010 Journal Article Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flowsKirchhartz, 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 |
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2009 Journal Article Boundary-layer separation due to combustion-induced pressure rise in a supersonic flowFrost, 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 |
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2008 Journal Article Numerical investigation of a spiked blunt nose cone at hypersonic speedsGauer, 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 |
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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 Journal Article Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight testHo, 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 |
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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 Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnelRobinson, 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 |
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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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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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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 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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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 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 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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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 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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1999 Journal Article Performance study of a power law starbodySabean, 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 |
