Professor Allan Paull

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

  • 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

  • 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.

  • 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

View all Publications

Grants

View all Grants

Supervision

View all Supervision

Publications

Journal Article

Conference Publication

  • 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.

  • 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

  • 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).

  • 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.

  • 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

  • Neuenhahn, Thomas, Olivier, Herbert and Paull, Allan (2006). Development of the HyShot stability demonstrator.

  • Coras, Samantha and Paull, Allan (2006). Experiments on external combustion with leading edge fuel-injection in hypersonic flow.

  • 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.

  • 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.

  • 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.

  • Mass, Neal E., Smart, Michael K. and Paull, Allan (2005). Flight data analysis of HyShot 2.

  • Finlayson, Simon and Paull, Allan (2005). A 256 channel high speed modular flight computer for hypersonic launch vehicles.

  • 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

  • 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.

  • 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

  • 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

  • Odam, J. and Paull, A. (2003). Comparison of experimental thrust measurements with theoretical values for a scramjet engine.

  • 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

  • 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.

  • 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

  • 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.

  • 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.

  • 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.

  • 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.

  • 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.

  • 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

  • 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

  • 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

  • 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.

  • 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.

  • 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.

  • 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.

  • 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

  • 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.

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

  • 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

Other Outputs

Grants (Administered at UQ)

PhD and MPhil Supervision

Completed Supervision