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
2002
Journal Article
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
2002
Conference Publication
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.
2002
Conference Publication
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.
2002
Conference Publication
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.
2002
Journal Article
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
2002
Conference Publication
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.
2002
Conference Publication
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.
2001
Conference Publication
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
2001
Journal Article
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
2001
Conference Publication
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
2000
Conference Publication
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
2000
Journal Article
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
2000
Journal Article
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
2000
Conference Publication
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.
2000
Conference Publication
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.
2000
Conference Publication
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.
2000
Journal Article
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
1999
Conference Publication
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.
1999
Journal Article
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
1999
Conference Publication
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
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
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