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
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
2006
Conference Publication
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.
2005
Conference Publication
Flight data analysis of HyShot 2
Mass, Neal E., Smart, Michael K. and Paull, Allan (2005). Flight data analysis of HyShot 2.
2005
Conference Publication
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.
2005
Conference Publication
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
2005
Journal Article
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
2005
Conference Publication
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.
2005
Conference Publication
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.
2004
Conference Publication
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
2004
Journal Article
Effects of hydrogen-air non-equilibrium chemistry on the performance of a model scramjet thrust nozzle
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
2004
Conference Publication
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
2003
Conference Publication
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.
2003
Journal Article
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.
2003
Conference Publication
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
2003
Journal Article
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
2003
Conference Publication
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.
2003
Conference Publication
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
2003
Conference Publication
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.
Funding
Current funding
Past funding
Supervision
Availability
- Professor Allan Paull is:
- Available for supervision
Before you email them, read our advice on how to contact a supervisor.
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
Enquiries
For media enquiries about Professor Allan Paull's areas of expertise, story ideas and help finding experts, contact our Media team: