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Professor Allan Paull

Chair in Future Hypersonic Technolo

School of Mechanical and Mining Engineering
Faculty of Engineering, Architecture and Information Technology

Chair in Future Hypersonic Technolo

School of Mechanical and Mining Engineering
Faculty of Engineering, Architecture and Information Technology
allan.paull@uq.edu.au
+61 7 336 53596

Overview

Qualifications

  • Masters (Coursework), The University of Queensland
  • Doctor of Philosophy, The University of Queensland
  • Bachelor (Honours) of Science (Advanced), The University of Queensland

Publications

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Grants

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Supervision

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Publications

Journal Article

Conference Publication

  • STAJe<sup>-</sup>: A Supersonic Flight Program STAJe-1 Payload Design and System Study

    Kunze, Jens, Shelar, Sampada Vijay and Paull, Allan (2024). STAJe-: A Supersonic Flight Program STAJe-1 Payload Design and System Study. AIAA Aviation Forum and Exposition (AIAA Aviation Forum), Chicago, IL United States, 27 June - 1 July 2022. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.A35544

  • System Overview of the STAJe<sup>-</sup> 1 Payload

    Kunze, Jens and Paull, Allan (2023). System Overview of the STAJe- 1 Payload. 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Karnataka, India, 28 May - 1 June 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-3004

  • 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

  • Investigation of an axisymmetric scramjet configuration utilising inlet-injection and radical farming

    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.

  • Radical farming in scramjets

    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.

  • Ground testing of the hyshot supersonic combustion flight experiment in HEG and comparison with flight data

    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.

  • Hyshot flight program

    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

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