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Professor

Allan Paull

Email: 
Phone: 
+61 7 336 53596

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

79 works between 1991 and 2024

41 - 60 of 79 works

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

Upstream porthole injection in a 2-D scramjet model

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.

Drag on a slender cone at mach 6.6 with film ejection of hydrogen

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.

Combustor and nozzle CFD calculations for the HyShot scramjet flight experiment

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.

In-situ sampling of gases and debris from volcanic plumes

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

Transducer for direct measurement of skin friction in hypervelocity impulse facilities

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.

Lift, pitching moment and thrust measurement on a fuelled scramjet

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.

Hyshot flight program

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

Viscous drag reduction in a scramjet combustor with film cooling

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

Skin-friction measurements in a supersonic combustor with crossflow fuel injection

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

Scramjet intake and exhaust CFD studies for the HyShot scramjet flight experiment

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

Pressure measurements in a scramjet combustor with film cooling

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

Hypervelocity skin-friction reduction by boundary-layer combustion of hydrogen

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

Unstarted inlet for direct-connect combustor experiments in a shock tunnel

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.

Simultaneous lift, moment and thrust measurement in hypervelocity flow

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.

Hypersonic airbreathing propulsion

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.

Hyshot scramjet testing in the T4 shock tunnel

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

Comparison of supersonic combustion beetween impulse and vitiation-heated facilities

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.

Upstream porthole injection in a 2-D scramjet model

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

Shock-tunnel skin-friction measurement in a supersonic combustor

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

Scram jet measurements in a shock tunnel

Funding

Current funding

  • 2023 - 2025
    Project STAJe
    MBDA UK Limited
    Open grant
  • 2022 - 2027
    Wind tunnel testing of a hypersonic plasma engine
    ARC Linkage Projects
    Open grant
  • 2021 - 2026
    STELaRLab for a Mach 4 Electric Engine
    Lockheed Martin Australia Pty Limited
    Open grant

Past funding

  • 2018 - 2023
    Chair in Future Hypersonic Technologies
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2010 - 2013
    Scramjet-based access-to-space systems
    Department of Innovation, Industry, Science and Research
    Open grant
  • 2006 - 2017
    Scramjet development from research to prototyping
    Queensland Government Smart State National and International Research Alliances Program
    Open grant
  • 2004 - 2005
    HyShot IV - JAXA Hypermixer Scramjet Flight Experiment (continuation of Hyshot prgram ref 2000100991)
    Japan Aerospace Exploration Agency
    Open grant
  • 2004 - 2005
    HyShot 8 - Ground testing and Flight test
    Department Defence - Defence Science & Technology
    Open grant
  • 2004
    Technology Maturation Study- Scramjet Propulsion and Control in Hypersonic Flight
    Department Defence - Defence Science & Technology
    Open grant
  • 2003 - 2004
    Mach 10 Scramjet Flight Thrust Measurements - An extension to the HyShot Flight Program
    United States National Aeronautics and Space Administration
    Open grant
  • 2002 - 2003
    Aerodynamic Heating Research
    Department Defence - Defence Science & Technology
    Open grant
  • 2001 - 2002
    Mach 7.6 Scramjet Flight Data and Data Analysis
    United States National Aeronautics and Space Administration
    Open grant
  • 2001 - 2003
    Flight Experimental Data from HYSHOT project, and extension with new title 'Design and Manufacturing Hypermixing and Development Works on Hypermixing Model and Hyshot Flight'
    Mitsubishi Heavy Industries Ltd
    Open grant
  • 2001 - 2006
    Hypersonic Airbreathing Propulsion Development.
    ARC Australian Senior Research Fellowships
    Open grant
  • 2001 - 2003
    Hypersonic airbreathing Propulsion Development - Combustor Drag Reduction.
    ARC Australian Research Council (Large grants)
    Open grant
  • 2001
    Radical Farm Development with Shock -Induced Ignition for Enhanced Hypersonic Airbreathing Propulson.
    University of Queensland Small Grants Scheme
    Open grant
  • 2000 - 2001
    Visit to the US and Japan to build productive commercial alliances with the international aerospace industry
    Department Industry Science & Resources
    Open grant
  • 2000 - 2001
    Investigations in The HyShot Flight Program
    United States Department of the Air Force (US Air Force)
    Open grant
  • 2000
    Lift produced by asymmetric combustion in a symmetric scramjet at angle of indicence.
    ARC Australian Research Council (Small grants)
    Open grant
  • 1999
    Shock tunnels test 2
    Defence Evaluation and Research Agency
    Open grant
  • 1999 - 2002
    Support for hydrocarbon combustion work
    Department Defence - Defence Science & Technology
    Open grant
  • 1999 - 2000
    Funding for the hyshot program under the apec market integration/industrial collaboration program
    Department Industry Science & Resources
    Open grant
  • 1999
    Scramjet shock tunnel tests
    Defence Evaluation and Research Agency
    Open grant
  • 1999 - 2001
    Simultaneous lift moment and thrust measurement in hypervelocity flow
    ARC Australian Research Council (Large grants)
    Open grant
  • 1999
    Skin friction in an operational scramjet combustor with film cooling
    ARC Australian Research Council (Small grants)
    Open grant
  • 1998 - 2001
    Scramjet ground test to flight test correlation
    United States National Aeronautics and Space Administration
    Open grant
  • 1998
    An Investigation into the Effect of Scale on Scramjets
    UQ External Support Enabling Grant
    Open grant
  • 1998
    Scramjet Collaboration with the DLR, Germany
    ARC Investigators - International Links
    Open grant
  • 1998
    Skin friction measurements in a scramjet with film cooling
    ARC Australian Research Council (Small grants)
    Open grant
  • 1997 - 1998
    Funding assistance for hypersonic facility
    DIST - Department Industry, Science and Tourism
    Open grant
  • 1997 - 1999
    Commissioning the superorbital expansion tube
    ARC Australian Research Council (Large grants)
    Open grant
  • 1997
    Kinetic Limited Combustion in a Scramjet
    ARC Australian Research Council (Small grants)
    Open grant
  • 1996 - 1997
    Collaboration with NASA on Scramjet Model Experiments
    Quality Funds Round 3
    Open grant
  • 1995 - 2000
    Hypervelocity propulsion
    ARC Australian Research Fellowship/QEII F/ship
    Open grant
  • 1995
    Scramjet combustion chamber skin friction measurement
    ARC Australian Research Council (Small grants)
    Open grant

Supervision

Availability

Professor Allan Paull is:
Available for supervision

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Supervision history

Current supervision

Completed supervision

Media

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