Overview
Availability
- Professor Allan Paull is:
- Available for supervision
Fields of research
Qualifications
- Bachelor (Honours) of Science (Advanced), The University of Queensland
- Doctor of Philosophy, The University of Queensland
- Masters (Coursework), The University of Queensland
Works
Search Professor Allan Paull’s works on UQ eSpace
2024
Journal Article
STAJe−: A supersonic flight program STAJe− 1 payload design and system study
Kunze, 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
2024
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
2023
Journal Article
Preliminary analysis of the performance of an electric supersonic propeller
Kunze, Jens and Paull, Allan (2023). Preliminary analysis of the performance of an electric supersonic propeller. Aerospace, 10 (9) 803, 803. doi: 10.3390/aerospace10090803
2023
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
2023
Conference Publication
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
2015
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.
2013
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
2012
Conference Publication
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).
2010
Journal Article
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
2009
Journal Article
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
2009
Conference Publication
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.
2009
Conference Publication
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
2008
Journal Article
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
2007
Conference Publication
Radical farming in scramjets
Odaml J. and Paull A. (2007). Radical farming in scramjets. doi: 10.1007/978-3-540-74460-3_34
2007
Conference Publication
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.
2006
Conference Publication
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.
2006
Conference Publication
Development of the HyShot stability demonstrator
Neuenhahn, Thomas, Olivier, Herbert and Paull, Allan (2006). Development of the HyShot stability demonstrator.
2006
Conference Publication
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.
2006
Journal Article
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
2006
Journal Article
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
Funding
Current funding
Past funding
Supervision
Availability
- Professor Allan Paull is:
- Available for supervision
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Supervision history
Current supervision
-
Doctor Philosophy
Experimental Investigation of Plasma Fuel Engine Performance
Associate Advisor
Other advisors: Dr Carolyn Jacobs, Professor Vincent Wheatley
Completed supervision
-
2013
Doctor Philosophy
Ethylene Augmentation of JP-8+100 in a Supersonic Combustor
Principal Advisor
Other advisors: Emeritus Professor David Mee
-
2011
Master Philosophy
Forebody Combustion Experiments on an Unducted Scramjet
Principal Advisor
Other advisors: Emeritus Professor David Mee
-
2007
Doctor Philosophy
HYSHOT SCRAMJET TESTING IN THE HEG
Principal Advisor
-
2006
Master Philosophy
ENHANCEMENT OF HYDROCARBON SUPERSONIC COMBUSTION BY RADICAL FARMING AND OXYGEN ENRICHMENT
Principal Advisor
-
2004
Doctor Philosophy
SCRAMJET EXPERIMENTS USING RADICAL FARMING
Principal Advisor
-
2003
Doctor Philosophy
SKIN FRICTION REDUCTION IN A COMBUSTION CHAMBER WITH FILM COOLING
Principal Advisor
Other advisors: Emeritus Professor David Mee
-
2010
Doctor Philosophy
An Experimental Investigation of Inlet Fuel Injection in a Three-Dimensional Scramjet Engine
Associate Advisor
-
2010
Doctor Philosophy
Investigation of an intake injected scramjet with a hot wall
Associate Advisor
Other advisors: Professor Tim McIntyre
-
2010
Doctor Philosophy
Upstream wall layer effects on drag reduction with boundary layer combustion
Associate Advisor
Other advisors: Emeritus Professor David Mee
-
2009
Doctor Philosophy
Nozzle optimization study and measurements for a quasi-axisymmetric scramjet model
Associate Advisor
Other advisors: Emeritus Professor David Mee
-
2007
Doctor Philosophy
STRUCTURE VERSUS FLEXIBILITY IN ENGINEERING DESIGN - THE TENSION BETWEEN DESIGN TOOLS AND CREATIVE PROBLEM SOLVING
Associate Advisor
-
2003
Doctor Philosophy
SIMULTANEOUS LIFT, MOMENT AND THRUST MEASUREMENT IN HYPERVELOCITY FLOW
Associate Advisor
Other advisors: Emeritus Professor David Mee
-
2002
Master Engineering Sc
Hyshot Scramjet Lift Evaluation
Associate Advisor
Other advisors: Emeritus Professor David Mee
Media
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