Other Outputs: Dataset for the Preliminary Analysis of the Performance of an Electric Supersonic Propeller
Kunze, Jens and Paull, Allan (2023). Dataset for the Preliminary Analysis of the Performance of an Electric Supersonic Propeller. The University of Queensland. (Dataset) doi: 10.48610/9292b60
Conference Publication: A concept for the HiFIRE 8 flight test
Alesi, Hans, Paull, Allan, Smart, Michael and Bowcutt, Kevin G. (2015). A concept for the HiFIRE 8 flight test. 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research, Tromso, Norway, 7-12 June 2015. Noordwijk, The Netherlands: ESA Communications.
Conference Publication: Ethylene augmentation of JP-8+100 in a supersonic combustor
Bateup, Mark L., Paull, Allan and Mee, David J. (2013). Ethylene augmentation of JP-8+100 in a supersonic combustor. JPC 2013: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, United States, 14-17 July, 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-3700
(2023–2025) MBDA UK Limited
Wind tunnel testing of a hypersonic plasma engine
(2022–2027) ARC Linkage Projects
STELaRLab for a Mach 4 Electric Engine
(2021–2025) Lockheed Martin Australia Pty Limited
Ethylene Augmentation of JP-8+100 in a Supersonic Combustor
(2013) Doctor Philosophy
Forebody Combustion Experiments on an Unducted Scramjet
(2011) Master Philosophy
HYSHOT SCRAMJET TESTING IN THE HEG
(2007) Doctor Philosophy
Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flows
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
Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow
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
Numerical investigation of a spiked blunt nose cone at hypersonic speeds
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
Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test
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
Flight data analysis of the HyShot 2 scramjet flight experiment
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
Performance of a scramjet combustor with combined normal and tangential fuel injection
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
Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnel
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
Scramjets and Shock Tunnels: The Queensland Experience
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
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. doi: 10.1017/S0001924000000403
Combustor and nozzle CFD calculations for the HyShot Scramjet flight experiment
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.
Skin-friction measurements in high-enthalpy hypersonic boundary layers
Goyne, 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
Upstream porthole injection in a 2-D scramjet model
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
Transducer for direct measurement of skin friction in hypervelocity impulse facilities
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
Skin-friction measurements in a supersonic combustor with crossflow fuel injection
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
Hypervelocity skin-friction reduction by boundary-layer combustion of hydrogen
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
Unstarted inlet for direct-connect combustor experiments in a shock tunnel
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
Comparison of supersonic combustion beetween impulse and vitiation-heated facilities
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
Performance study of a power law starbody
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
Shock-tunnel skin-friction measurement in a supersonic combustor
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
Experiments on cruise propulsion with a hydrogen scramjet
Stalker R.J. and Paull A. (1998). Experiments on cruise propulsion with a hydrogen scramjet. Aeronautical Journal, 102 (1011), 37-43.
A driver gas detection device for shock tunnels
Paull A. and King M.D. (1995). A driver gas detection device for shock tunnels. Shock Waves, 4 (5), 289-291. doi: 10.1007/BF01416041
Experiments on supersonic combustion ramjet propulsion in a shock tunnel
Paull A., Stalker R.J. and Mee D.J. (1995). Experiments on supersonic combustion ramjet propulsion in a shock tunnel. Journal of Fluid Mechanics, 296 (-1), 159-183. doi: 10.1017/S0022112095002096
Scramjet thrust measurement in a shock tunnel
Paull A., Stalker R.J. and Mee D.J. (1995). Scramjet thrust measurement in a shock tunnel. Aeronautical Journal, 99 (984), 161-163. doi: 10.1017/s0001924000027147
Shock tunnel measurements of hypervelocity blunted cone drag
Porter L.M., Paull A., Mee D.J. and Simmons J.M. (1994). Shock tunnel measurements of hypervelocity blunted cone drag. AIAA journal, 32 (12), 2476-2477. doi: 10.2514/3.12318
Skin-friction gauge for use in hypervelocity impulse facilities
Kelly G.M., Simmons J.M. and Paull A. (1992). Skin-friction gauge for use in hypervelocity impulse facilities. AIAA journal, 30 (3), 844-845. doi: 10.2514/3.10996
Test flow disturbances in an expansion tube
Paull A. and Stalker R.J. (1992). Test flow disturbances in an expansion tube. Journal of Fluid Mechanics, 245 (-1), 493-521. doi: 10.1017/S0022112092000569
The effect on an acoustic wave as it traverses an unsteady expansion
Paull A. and Stalker R.J. (1991). The effect on an acoustic wave as it traverses an unsteady expansion. Physics of Fluids A, 3 (4), 717-719. doi: 10.1063/1.858079
A concept for the HiFIRE 8 flight test
Alesi, Hans, Paull, Allan, Smart, Michael and Bowcutt, Kevin G. (2015). A concept for the HiFIRE 8 flight test. 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research, Tromso, Norway, 7-12 June 2015. Noordwijk, The Netherlands: ESA Communications.
Ethylene augmentation of JP-8+100 in a supersonic combustor
Bateup, Mark L., Paull, Allan and Mee, David J. (2013). Ethylene augmentation of JP-8+100 in a supersonic combustor. JPC 2013: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, United States, 14-17 July, 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-3700
HIFiRE: an international collaboration to advance the science and technology of hypersonic flight
Bowcutt, Kevin, Paull, Alan, Dolvin, Douglas and Smart, Michael (2012). HIFiRE: an international collaboration to advance the science and technology of hypersonic flight. 28th International Congress of the Aeronautical Sciences (ICAS 2012), Brisbane, QLD, Australia, 23-28 September 2012. Bonn, Germany: International Council of the Aeronautical Sciences (ICAS).
Aerodynamic design of hypersonic re-entry flight HIFiRE 7
Eggers, Thino, Silvester, Todd B., Paull, Allan and Smart, Michael K. (2009). Aerodynamic design of hypersonic re-entry flight HIFiRE 7. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, 19 - 22 October 2009. Reston, VA United States: AIAA. doi: 10.2514/6.2009-7256
Hunt, D. C., Paull, A., Boyce, R. R. and Hagenmaier, M. (2009). Investigation of an axisymmetric scramjet configuration utilising inlet-injection and radical farming. 19th International Symposium on Airbreathing Engines (ISABE2009), Montreal, Canada, 7-11 September, 2009. Montreal, Canada: ISABE.
Hypersonics Research in Australia
Morgan, Richard, Paull, Allan, Smart, Michael and Stalker, Ray (2007). Hypersonics Research in Australia. 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, 12-15 March 2007. Neuilly-sur-Seine, France: NATO Research and Technology Organisation.
Odaml J. and Paull A. (2007). Radical farming in scramjets. doi: 10.1007/978-3-540-74460-3_34
Development of the HyShot stability demonstrator
Neuenhahn, Thomas, Olivier, Herbert and Paull, Allan (2006). Development of the HyShot stability demonstrator.
Experiments on external combustion with leading edge fuel-injection in hypersonic flow
Coras, Samantha and Paull, Allan (2006). Experiments on external combustion with leading edge fuel-injection in hypersonic flow.
Development of the Hyshot Stability Demonstrator
Neuenhahn, 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.
Experiments on external combusion with leading edge fuel-injection in hypersonic flow
Coras, 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.
Imaging of hydrogen fuel injection on the intake of a heated wall scramjet
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. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Sacramento, California, 9 - 12 July 2006. AIAA.
Flight data analysis of HyShot 2
Mass, Neal E., Smart, Michael K. and Paull, Allan (2005). Flight data analysis of HyShot 2.
A 256 channel high speed modular flight computer for hypersonic launch vehicles
Finlayson, Simon and Paull, Allan (2005). A 256 channel high speed modular flight computer for hypersonic launch vehicles.
Performance of a scramjet combustor with combined normal and tangential fuel injection
Rowan, 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
Flight Data Analysis of HyShot 2
Hass, 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.
Operating conditions in UQ's impulse facilities for scramjet testing
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. 25th International Symposium on Shock Waves, Bangalore, India, 17-22 July 2005.
Gardner, 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
Investigation of an intake injected hot-wall scramjet
Kovachevich, 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
Comparison of experimental thrust measurements with theoretical values for a scramjet engine
Odam, J. and Paull, A. (2003). Comparison of experimental thrust measurements with theoretical values for a scramjet engine.
CFD calculations for intake-injection shock-induced-combustion scramjet flight experiments
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. 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
Measurement of the aerodynamic performance of a scramjet-powered vehicle in a shock tunnel
Robinson, 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.
The HyShot Scramjet Flight Experiment - Flight Data and CFD Calculations Compared
Boyce, 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
The Methodology behind the Hyshot Flight Program
Paull, 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.
Combustor and nozzle CFD calculations for the HyShot scramjet flight experiment
Boyce, 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.
Drag on a slender cone at mach 6.6 with film ejection of hydrogen
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. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23.
Paull, 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.
In-situ sampling of gases and debris from volcanic plumes
Takayama, 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.
Lift, pitching moment and thrust measurement on a fuelled scramjet
Robinson, 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.
Viscous drag reduction in a scramjet combustor with film cooling
Rowan, 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
Scramjet intake and exhaust CFD studies for the HyShot scramjet flight experiment
Boyce 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
Pressure measurements in a scramjet combustor with film cooling
Rowan, 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
Hypersonic airbreathing propulsion
Paull, A. (2000). Hypersonic airbreathing propulsion. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton.
Hyshot scramjet testing in the T4 shock tunnel
Frost, 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.
Simultaneous lift, moment and thrust measurement in hypervelocity flow
Robinson, 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.
Intake design for a scramjet flight experiment
Boyce, 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.
Scram jet measurements in a shock tunnel
Paull 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
Upstream porthole injection in a 2-D scramjet model
Gardner, 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.
A joint American-Australian university hypersonic research program
Lewis M.J. and Paull A. (1998). A joint American-Australian university hypersonic research program. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-1551
Performance study of a power law star body
Sabean, John W., Lewis, Mark J., Mee, David and Paull, Allan (1998). Performance study of a power law star body. 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 1998, Norfolk, VA, April 27, 1998-April 30, 1998. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-1617
Scramjet testing in the T4 impulse facility
Paull A. and Stalker R.J. (1998). Scramjet testing in the T4 impulse facility. 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 1998, April 27, 1998-April 30, 1998. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-1533
Shock tunnel skin friction measurement in a supersonic combustor
Goyne, C. P., Stalker, R. J. and Paull, A. (1998). Shock tunnel skin friction measurement in a supersonic combustor. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-943
Supersonic combustion - A shock tunnel and vitiation-heated slowdown tunnel comparison
Boyce R.R., Wendt M., Paull A., Chinzei N., Stalker R.J. and Miyajima H. (1998). Supersonic combustion - A shock tunnel and vitiation-heated slowdown tunnel comparison. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-941
A shock tunnel investigation of scramjet performance with partially premixed combustion
Stalker, R.J., Morgan, R.G. and Paull, A. (1996). A shock tunnel investigation of scramjet performance with partially premixed combustion. Space Plane and Hypersonic Systems and Technology Conference, 1996, *, 18-22 November 1996. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1996-4534
A skin friction gauge for impulsive flows
Goyne C.P., Paull A. and Stalker R.J. (1995). A skin friction gauge for impulsive flows. 31st Joint Propulsion Conference and Exhibit, 1995, July 10, 1995-July 12, 1995. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1995-3152
Measurement of Scramjet Thrust in Shock Tunnels
Stalker, R. J., Simmons, J. M., Paull, A. and Mee, D. J. (1994). Measurement of Scramjet Thrust in Shock Tunnels. AIAA 18th Aerospace Ground Testing Conference, Colorado Springs, Colorado, USA, 20-23 June, 1994. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1994-2516
Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility
Paull, A., Stalker, R. J. and Mee, D. J. (1993). Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility. AIAA and DGLR, 5th International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, 30 November - 3 December, 1993. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1993-5168
Dataset for the Preliminary Analysis of the Performance of an Electric Supersonic Propeller
Kunze, Jens and Paull, Allan (2023). Dataset for the Preliminary Analysis of the Performance of an Electric Supersonic Propeller. The University of Queensland. (Dataset) doi: 10.48610/9292b60
(2023–2025) MBDA UK Limited
Wind tunnel testing of a hypersonic plasma engine
(2022–2027) ARC Linkage Projects
STELaRLab for a Mach 4 Electric Engine
(2021–2025) Lockheed Martin Australia Pty Limited
Chair in Future Hypersonic Technologies
(2018–2023) Commonwealth Defence Science and Technology Group
Scramjet-based access-to-space systems
(2010–2013) Department of Innovation, Industry, Science and Research
Scramjet development from research to prototyping
(2006–2017) Queensland Government Smart State National and International Research Alliances Program
HyShot 8 - Ground testing and Flight test
(2004–2005) Department Defence - Defence Science & Technology
(2004–2005) Japan Aerospace Exploration Agency
Technology Maturation Study- Scramjet Propulsion and Control in Hypersonic Flight
(2004) Department Defence - Defence Science & Technology
Mach 10 Scramjet Flight Thrust Measurements - An extension to the HyShot Flight Program
(2003–2004) United States National Aeronautics and Space Administration
(2002–2003) Department Defence - Defence Science & Technology
Hypersonic Airbreathing Propulsion Development.
(2001–2006) ARC Australian Senior Research Fellowships
(2001–2003) Mitsubishi Heavy Industries Ltd
Hypersonic airbreathing Propulsion Development - Combustor Drag Reduction.
(2001–2003) ARC Australian Research Council (Large grants)
Mach 7.6 Scramjet Flight Data and Data Analysis
(2001–2002) United States National Aeronautics and Space Administration
(2001) University of Queensland Small Grants Scheme
Investigations in The HyShot Flight Program
(2000–2001) United States Department of the Air Force (US Air Force)
(2000–2001) Department Industry Science & Resources
Lift produced by asymmetric combustion in a symmetric scramjet at angle of indicence.
(2000) ARC Australian Research Council (Small grants)
Support for hydrocarbon combustion work
(1999–2002) Department Defence - Defence Science & Technology
Simultaneous lift moment and thrust measurement in hypervelocity flow
(1999–2001) ARC Australian Research Council (Large grants)
Funding for the hyshot program under the apec market integration/industrial collaboration program
(1999–2000) Department Industry Science & Resources
(1999) Defence Evaluation and Research Agency
(1999) Defence Evaluation and Research Agency
Skin friction in an operational scramjet combustor with film cooling
(1999) ARC Australian Research Council (Small grants)
Scramjet ground test to flight test correlation
(1998–2001) United States National Aeronautics and Space Administration
An Investigation into the Effect of Scale on Scramjets
(1998) UQ External Support Enabling Grant
Scramjet Collaboration with the DLR, Germany
(1998) ARC Investigators - International Links
Skin friction measurements in a scramjet with film cooling
(1998) ARC Australian Research Council (Small grants)
Commissioning the superorbital expansion tube
(1997–1999) ARC Australian Research Council (Large grants)
Funding assistance for hypersonic facility
(1997–1998) DIST - Department Industry, Science and Tourism
Kinetic Limited Combustion in a Scramjet
(1997) ARC Australian Research Council (Small grants)
Collaboration with NASA on Scramjet Model Experiments
(1996–1997) Quality Funds Round 3
(1995–2000) ARC Australian Research Fellowship/QEII F/ship
Scramjet combustion chamber skin friction measurement
(1995) ARC Australian Research Council (Small grants)
Experimental Investigation of Plasma Fuel Engine Performance
Doctor Philosophy — Associate Advisor
Other advisors:
Ethylene Augmentation of JP-8+100 in a Supersonic Combustor
(2013) Doctor Philosophy — Principal Advisor
Other advisors:
Forebody Combustion Experiments on an Unducted Scramjet
(2011) Master Philosophy — Principal Advisor
Other advisors:
HYSHOT SCRAMJET TESTING IN THE HEG
(2007) Doctor Philosophy — Principal Advisor
ENHANCEMENT OF HYDROCARBON SUPERSONIC COMBUSTION BY RADICAL FARMING AND OXYGEN ENRICHMENT
(2006) Master Philosophy — Principal Advisor
SCRAMJET EXPERIMENTS USING RADICAL FARMING
(2004) Doctor Philosophy — Principal Advisor
SKIN FRICTION REDUCTION IN A COMBUSTION CHAMBER WITH FILM COOLING
(2003) Doctor Philosophy — Principal Advisor
Other advisors:
An Experimental Investigation of Inlet Fuel Injection in a Three-Dimensional Scramjet Engine
(2010) Doctor Philosophy — Associate Advisor
Investigation of an intake injected scramjet with a hot wall
(2010) Doctor Philosophy — Associate Advisor
Other advisors:
Upstream wall layer effects on drag reduction with boundary layer combustion
(2010) Doctor Philosophy — Associate Advisor
Other advisors:
Nozzle optimization study and measurements for a quasi-axisymmetric scramjet model
(2009) Doctor Philosophy — Associate Advisor
Other advisors:
STRUCTURE VERSUS FLEXIBILITY IN ENGINEERING DESIGN - THE TENSION BETWEEN DESIGN TOOLS AND CREATIVE PROBLEM SOLVING
(2007) Doctor Philosophy — Associate Advisor
SIMULTANEOUS LIFT, MOMENT AND THRUST MEASUREMENT IN HYPERVELOCITY FLOW
(2003) Doctor Philosophy — Associate Advisor
Other advisors:
Hyshot Scramjet Lift Evaluation
(2002) Master Engineering Sc — Associate Advisor
Other advisors: