Professor

Allan Paull

Email: 
Phone: 
+61 7 336 53596

Availability

Professor Allan Paull is:
Available for supervision

Fields of research

Engineering

Qualifications

  • Bachelor (Honours) of Science (Advanced), The University of Queensland
  • Doctor of Philosophy, The University of Queensland
  • Masters (Coursework), The University of Queensland

Search Professor Allan Paull’s works on UQ eSpace

79 works between 1991 and 2024
All (79) Journal Article (29) Conference Publication (49) Other Outputs (1)

61 - 79 of 79 works

1999

Conference Publication

Intake design for a scramjet flight experiment

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.

Intake design for a scramjet flight experiment

1999

Journal Article

Performance study of a power law starbody

Sabean, JW, Lewis, MJ, Mee, D and Paull, A (1999). Performance study of a power law starbody. Journal of Spacecraft and Rockets, 36 (5), 646-652. doi: 10.2514/2.3496

Performance study of a power law starbody

1998

Conference Publication

Performance study of a power law star body

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

Performance study of a power law star body

1998

Conference Publication

Supersonic combustion - A shock tunnel and vitiation-heated slowdown tunnel comparison

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

Supersonic combustion - A shock tunnel and vitiation-heated slowdown tunnel comparison

1998

Journal Article

Experiments on cruise propulsion with a hydrogen scramjet

Stalker R.J. and Paull A. (1998). Experiments on cruise propulsion with a hydrogen scramjet. Aeronautical Journal, 102 (1011), 37-43.

Experiments on cruise propulsion with a hydrogen scramjet

1998

Conference Publication

A joint American-Australian university hypersonic research program

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

A joint American-Australian university hypersonic research program

1998

Conference Publication

Scramjet testing in the T4 impulse facility

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

Scramjet testing in the T4 impulse facility

1998

Conference Publication

Shock tunnel skin friction measurement in a supersonic combustor

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

Shock tunnel skin friction measurement in a supersonic combustor

1996

Conference Publication

A shock tunnel investigation of scramjet performance with partially premixed combustion

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

A shock tunnel investigation of scramjet performance with partially premixed combustion

1995

Journal Article

A driver gas detection device for shock tunnels

Paull A. and King M.D. (1995). A driver gas detection device for shock tunnels. Shock Waves, 4 (5), 289-291. doi: 10.1007/BF01416041

A driver gas detection device for shock tunnels

1995

Conference Publication

A skin friction gauge for impulsive flows

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

A skin friction gauge for impulsive flows

1995

Journal Article

Scramjet thrust measurement in a shock tunnel

Paull A., Stalker R.J. and Mee D.J. (1995). Scramjet thrust measurement in a shock tunnel. Aeronautical Journal, 99 (984), 161-163. doi: 10.1017/s0001924000027147

Scramjet thrust measurement in a shock tunnel

1995

Journal Article

Experiments on supersonic combustion ramjet propulsion in a shock tunnel

Paull A., Stalker R.J. and Mee D.J. (1995). Experiments on supersonic combustion ramjet propulsion in a shock tunnel. Journal of Fluid Mechanics, 296 (-1), 159-183. doi: 10.1017/S0022112095002096

Experiments on supersonic combustion ramjet propulsion in a shock tunnel

1994

Conference Publication

Measurement of Scramjet Thrust in Shock Tunnels

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

Measurement of Scramjet Thrust in Shock Tunnels

1994

Journal Article

Shock tunnel measurements of hypervelocity blunted cone drag

Porter L.M., Paull A., Mee D.J. and Simmons J.M. (1994). Shock tunnel measurements of hypervelocity blunted cone drag. AIAA journal, 32 (12), 2476-2477. doi: 10.2514/3.12318

Shock tunnel measurements of hypervelocity blunted cone drag

1993

Conference Publication

Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility

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

Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility

1992

Journal Article

Test flow disturbances in an expansion tube

Paull A. and Stalker R.J. (1992). Test flow disturbances in an expansion tube. Journal of Fluid Mechanics, 245 (-1), 493-521. doi: 10.1017/S0022112092000569

Test flow disturbances in an expansion tube

1992

Journal Article

Skin-friction gauge for use in hypervelocity impulse facilities

Kelly G.M., Simmons J.M. and Paull A. (1992). Skin-friction gauge for use in hypervelocity impulse facilities. AIAA journal, 30 (3), 844-845. doi: 10.2514/3.10996

Skin-friction gauge for use in hypervelocity impulse facilities

1991

Journal Article

The effect on an acoustic wave as it traverses an unsteady expansion

Paull A. and Stalker R.J. (1991). The effect on an acoustic wave as it traverses an unsteady expansion. Physics of Fluids A, 3 (4), 717-719. doi: 10.1063/1.858079

The effect on an acoustic wave as it traverses an unsteady expansion

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

Availability

Professor Allan Paull is:
Available for supervision

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Supervision history

Current supervision

Completed supervision

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