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)

1 - 20 of 79 works

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

STAJe<sup>-</sup>: A Supersonic Flight Program STAJe-1 Payload Design and System Study

2024

Journal Article

STAJe−: A supersonic flight program STAJe− 1&nbsp;payload design and system study

Kunze, Jens, Vijay Shelar, Sampada and Paull, Allan (2024). STAJe−: A supersonic flight program STAJe− 1&nbsp;payload design and system study. Journal of Spacecraft and Rockets, 61 (1), 233-247. doi: 10.2514/1.a35544

STAJe−: A supersonic flight program STAJe− 1&nbsp;payload design and system study

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. doi: 10.3390/aerospace10090803

Preliminary analysis of the performance of an electric supersonic propeller

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

Dataset for the Preliminary Analysis of the Performance of an Electric Supersonic Propeller

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

System Overview of the STAJe<sup>-</sup> 1 Payload

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.

A concept for the HiFIRE 8 flight test

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

Ethylene augmentation of JP-8+100 in a supersonic combustor

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).

HIFiRE: an international collaboration to advance the science and technology of hypersonic flight

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

Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flows

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

Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow

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

Aerodynamic design of hypersonic re-entry flight HIFiRE 7

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.

Investigation of an axisymmetric scramjet configuration utilising inlet-injection and radical farming

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

Numerical investigation of a spiked blunt nose cone at hypersonic speeds

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.

Hypersonics Research in Australia

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

Radical farming in scramjets

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.

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.

Development of the HyShot stability demonstrator

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

Flight data analysis of the HyShot 2 scramjet flight experiment

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.

Experiments on external combusion with leading edge fuel-injection in hypersonic flow

2006

Journal Article

Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test

Ho, S. Y. and Paull, A. (2006). Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test. Aerospace Science And Technology, 10 (5), 420-426. doi: 10.1016/j.ast.2006.03.004

Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test

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 - 2025
    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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