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Associate Professor Vincent Wheatley

Associate Professor

School of Mechanical and Mining Engineering
Faculty of Engineering, Architecture and Information Technology
v.wheatley@uq.edu.au
+61 7 336 52969

Overview

Dr Wheatley is the Chair of Teaching and Learning for the School of Mechanical and Mining Engineering. He is a member of the Centre for Hyperosonics and was named Australia's Research Field Leader in Aerospace and Aviation Engineering (The Australian, Sept 28, 2018). He was a recipient of a 2017 Australian Award for University Teaching – Award for Teaching Excellence .

Dr Wheatley's research interests are in the fields of supersonic plasma flows, hypersonics and computational fluid dynamics.

Dr Wheatley's research in supersonic plasma flows focuses on the suppression of instabilities that are detrimental to inertial confinement fusion, a process that promises carbon free energy production. In hypersonics, he focuses on extending the capability scramjets to the point where they can power launch-vehicle stages. This technology could meet the need for safer, more economical space access, which has the potential to revolutionise the space industry. Computational fluid dynamics is his primary method of investigation in these areas.

Dr Wheatley obtained his PhD in Aeronautics from the California Institute of Technology in 2005. He also earned an MEngSc (Mechanical) and a BE (Mechanical and Space) from the University of Queensland (UQ). After completing his PhD in the US, Dr Wheatley spent two years as post-doctoral fellow at ETH Zurich. He was then a Lecturer in Aerospace Engineering at the University of Adelaide before taking up his position at UQ in 2009.

Dr Wheatley has expertise in the areas of:

  • Simulation of hypersonic flows (DNS, LES and RANS)
  • Using high fidelity numerical simulations, validated by experiments, to provide new details and understanding of scramjet flow physics
  • Mixing and combustion enhancement in scramjets through fuel/flow structure interactions and novel injector design
  • Analysis and simulation of plasma instabilities
  • Numerical methods for magnetohydrodynamics (MHD) and multi-fluid, ion-electron plasmas
  • Rarefied gas dynamics
  • Bluff body wake dynamics
  • Aeroacoustics, particularly passive noise control for bluff bodies

Qualifications

  • Bachelor of Engineering with Honours, The University of Queensland
  • Master of Engineering Science (Mechanical), The University of Queensland
  • Doctor of Philosophy, California Institute of Technology

Publications

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Grants

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Supervision

  • Investigation of flow field manipulation, thermal compression and mode transition in a Mach 5-10 scramjet accelerator

    Doctor Philosophy

  • Simulation and Dynamics of Hypersonic Turbulent Combustion

    (2019) Doctor Philosophy

  • Two-fluid modeling of electron transpiration cooling for the leading edges of hypersonic vehicles

    Doctor Philosophy

View all Supervision

Available Projects

  • Numerical investigation of scramjet acoustic loads

    Acoustic loads in hypersonic air-breathing engines have been recognized as a serious issue since the 1980s, yet their mitigation remains an open problem. With the successful X51 flight tests at low hypersonic Mach numbers and our success in the laboratory at up to Mach 12, resolving the remaining technical barriers to developing reusable hypersonic vehicles has gained immediate importance. The first step towards effective mitigation or management of scramjet acoustic loads is to develop the capability to accurately predict and understand them. It is this important problem that the proposed research aims to address as part of the 2017 ARC Discovery Project “Acoustic loads on hypersonic vehicles”.

    The primary goal of this PhD project is to conduct Wall-Modelled Large-Eddy Simulation (WMLES) of the supersonic and hypersonic experiments conducted by other students, then through comparison of the numerical and experimental acoustic data, refine the simulation approach and ultimately validate it. Once the simulation approach has been validated, WMLES will provide highly detailed, time accurate data upon which to build our understanding of the sound generation mechanisms in scramjets. The approach will also be able to accurately predict the acoustic loads in other supersonic engines.

  • Two-fluid MHD investigation of the magnetic suppression of shock driven plasma instabilities

    In inertial confinement fusion, hundreds of terawatts of laser power is used to drive a converging shock wave into a small spherical capsule containing a fuel mixture of heavy hydrogen isotopes. When the shock wave converges at the centre of the capsule, the temperature should exceed 100 million Kelvin and a fusion reaction between the hydrogen nuclei should be ignite. The fusion burn should then propagate outward through the fuel more rapidly than it can expand. However, when the shock impacts on the interfaces between the capsule and the fuel layers, hydrodynamic instabilities are triggered. The first of these is the Richtmyer-Meshkov instability, which occurs when a shock interacts with a density interface. The hydrodynamic instabilities limit the chance of energy break-even or production.

    In the last few years, we have shown that in ideal plasmas, the Richtmyer-Meshkov instability can be suppressed by the application of a seed magnetic field. The extreme temperatures involved in inertial confinement fusion mean the fluids involved are plasmas, so suppressing the instability is possible. Unfortunately, to suppress the instability and maintain spherical symmetry would require a radial magnetic field, which is not attainable. Instead we have studied cases where the instability is suppressed using realistic magnetic fields, with very promising results.

    The results discussed above were obtained using ideal magnetohydrodynamics (MHD), which is one of the simplest frameworks for modelling plasma behaviour. In this project, the suppression of the Richtmyer-Meskov instability will be investigated using the more realistic framework of two-fluid MHD, where the electrons and heavy ions are simulated separately, and the full set of Maxwell's equations are solved to determine the evolution of the electric and magnetic fields. This framework allows a wealth of plasma behaviour that cannot occur in ideal MHD. The crucial outcome of this project will be to determine how these phenomena affect the suppression of the Ritchmyer-Meshkov instability in the presence of a seed magnetic field.

  • Experimental investigation of scramjet acoustic loads

    Acoustic loads in hypersonic air-breathing engines have been recognized as a serious issue since the 1980s, yet their mitigation remains an open problem. With the successful X51 flight tests at low hypersonic Mach numbers and our success in the laboratory at up to Mach 12, resolving the remaining technical barriers to developing reusable hypersonic vehicles has gained immediate importance. An essential step towards effective mitigation or management of scramjet acoustic loads is to measure them in a realistic environment, providing vital data to validate predictive models. It is this important problem that the proposed research aims to address as part of the 2017 ARC Discovery Project “Acoustic loads on hypersonic vehicles”.

    The primary goal of this PhD project is experimentally measure acoustic loads in a scramjet engine under realistic hypersonic flight and fuel injection conditions in UQ’s T4 Shock Tunnel. This facility can faithfully recreate the flow physics in scramjet engines, including the acoustic environment. The experimental measurement of acoustic waves in shock tunnels is extremely challenging: The impact of the free-piston driver, diaphragm bursting and transient shock reflections produce intense structural vibrations. Test flows at multiple kilometers per second are generated with stagnation temperatures of over 5000 K. Many of the sensors typically used in aeroacoustics cannot withstand this extreme thermal environment. We will overcome these limitations and resolve all waves above 5 kHz by using the focused laser differential interferometer (FLDI) technique. This method has been proven to work in the T5 shock tunnel in Caltech for external flows; this will be the first application to scramjet flows in a reflected shock tunnel. The method will be extended to simultaneously measure perturbations at three locations, enabling acoustic signals to be distinguished from entropy waves. The proposed experimental design will produce a supersonic turbulent reacting flow with features that closely match those in a candidate access-to-space scramjet. Using FLDI to probe the sound field at key points will permit a high-fidelity, time-resolved comparison between experimental and numerical data for validation purposes.

View all Available Projects

Publications

Journal Article

Conference Publication

  • Fundamental scramjet combustion experiments using hydrocarbon fuel

    Vanyai, Tristan, Grieve, Sam, Street, Oliver, Denman, Zachary, McIntyre, Timothy, Veeraragavan, Ananthanarayanan, Wheatley, Vincent and Smart, Michael (2019). Fundamental scramjet combustion experiments using hydrocarbon fuel. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.B37472

  • Investigating the two-fluid plasma Richtmyer-Meshkov instability: a tale of two codes

    Bond, D., Wheatley, V., Samtaney, R. and Li, Y. (2019). Investigating the two-fluid plasma Richtmyer-Meshkov instability: a tale of two codes. ISSW32: 32nd International Symposium on Shock Waves, Singapore, 14-19 July 2019. Singapore: Research Publishing, Singapore. doi: 10.3850/978-981-11-2730-4_0169-cd

  • Investigation of combustion mode control in a Mach 8 shape-transitioning scramjet

    Curran, Damian, Wheatley, Vincent and Smart, Michael (2019). Investigation of combustion mode control in a Mach 8 shape-transitioning scramjet. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, Orlando Fl, Sep 17-19, 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.j057999

  • Tailored Fuel Injection for Performance Enhancement in a Mach 12 Scramjet Engine

    Barth, James E., Wise, Dylan J., Wheatley, Vincent and Smart, Michael K. (2019). Tailored Fuel Injection for Performance Enhancement in a Mach 12 Scramjet Engine. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, Jul 06-09, 2015. Reston, VA, United States : American Institute of Aeronautics and Astronautics. doi: 10.2514/1.B36794

  • The Richtmyer-Meshkov instability of an isotope interface in a two-fluid plasma

    Bond, Daryl, Wheatley, Vincent, Samtaney, Ravi, Li, Yuan and Pullin, Dale (2019). The Richtmyer-Meshkov instability of an isotope interface in a two-fluid plasma. 32nd International Symposium on Shock Waves, Singapore, 14-19 July 2019. Singapore: Research Publishing, Singapore. doi: 10.3850/978-981-11-2730-4_0170-cd

  • Simulation of laser-Induced plasma ignition in a hypersonic crossflow

    Gibbons, Nicholas, Gehre, Rolf, Brieschenk, Stefan and Wheatley, Vincent (2018). Simulation of laser-Induced plasma ignition in a hypersonic crossflow. Reston, VA United States: American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.j055821

  • Fundamental scramjet combustion experiments using hydrocarbon fuel

    Vanyai, Tristan, Grieve, Sam, Street, Oliver, Denman, Zachary, McIntyre, Timothy, Veeraragavan, Anand, Wheatley, Vincent and Smart, Michael (2018). Fundamental scramjet combustion experiments using hydrocarbon fuel. AIAA International Space Planes and Hypersonics Systems and Technologies Conference, AIAA SPACE Forum, Orlando, FL, United States, 17–19 September 2018. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-5201

  • Investigation of combustion mode control in a mach 8 shape-transitioning scramjet

    Curran, Damian R., Wheatley, Vincent and Smart, Michael K. (2018). Investigation of combustion mode control in a mach 8 shape-transitioning scramjet. 2018 AIAA SPACE and Astronautics Forum and Exposition, Orlando, Florida, 17-19 September 2018. Reston, Virginia: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-5380

  • Magnetohydrodynamic drag force measurements in an expansion tube

    Smith, Daniel R., Gildfind, David E., James, Christopher M., McIntyre, Timothy J. and Wheatley, Vincent (2018). Magnetohydrodynamic drag force measurements in an expansion tube. 9th AIAA Flow Control Conference 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-3755

  • Simulation of forced ignition in a Mach 6 scramjet combustor

    Curran, D. R., Wheatley, V. and Smart, M. K. (2018). Simulation of forced ignition in a Mach 6 scramjet combustor. Australasian Fluid Mechanics Conference, Adelaide, Australia, 10-13 December 2018. Perth, WA, United States: Australasian Fluid Mechanics Society.

  • Sound generation by a supersonic reacting mixing layer

    Cartmill, I., Gibbons, N., Wheatley, V. and Doolan, C. (2018). Sound generation by a supersonic reacting mixing layer. Australasian Fluid Mechanics Conference, Adelaide, Australia, 10-13 December 2018. Perth, WA, United States: Australasian Fluid Mechanics Society.

  • Flow field manipulation via fuel injectors in scramjets

    Landsberg, Will O., Gibbons, Nicholas N., Wheatley, Vincent, Smart, Michael K. and Veeraragavan, Ananthanarayanan (2017). Flow field manipulation via fuel injectors in scramjets. 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, 6 - 9 March 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics.

  • Performance of high Mach number scramjets - Tunnel vs flight

    Landsberg, Will O., Wheatley, Vincent, Smart, Michael and Veeraragavan, Ananthanarayanan (2017). Performance of high Mach number scramjets - Tunnel vs flight. 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017, Adelaide, SA, Australia, 25-29 September 2017. Paris, France: International Astronautical Federation.

  • Reducing combustor length within a mach 12 shape-transitioning scramjet

    Landsberg, Will O., Wheatley, Vincent, Smart, Michael K and Veeraragavan, Ananthanarayanan (2017). Reducing combustor length within a mach 12 shape-transitioning scramjet. 11th Asia-Pacific Conference on Combustion, ASPACC 2017, Sydney, Australia, 10-14 December 2017. Sydney, Australia: Combustion Institute.

  • Fuel injection and mixing in a Mach 8 hydrocarbon-fuelled scramjet

    Denman, Z. J., Wheatley, V., Smart, M. K. and Veeraragavan, A . (2016). Fuel injection and mixing in a Mach 8 hydrocarbon-fuelled scramjet. 20th Australasian Fluid Mechanics Conference, Perth, Australia, 5 – 8 December 2016. Perth, Australia: Australasian Fluid Mechanics Society.

  • Local field effects on magnetic suppression of the converging Richtmyer-Meshkov instability

    Wheatley, V., Mostert, W., Bond, D. M. and Samtaney, R. (2016). Local field effects on magnetic suppression of the converging Richtmyer-Meshkov instability. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, 5-8 December 2016. Victoria, Australia: Australasian Fluid Mechanics Society.

  • On the development of a Mach 10 scramjet engine for investigation of supersonic combustion regimes

    Moura, A. F., Wheatley, V., McIntyre, T. J. and Jahn, I. (2016). On the development of a Mach 10 scramjet engine for investigation of supersonic combustion regimes. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, 5-8 December 2016. Victoria, Australia: Australasian Fluid Mechanics Society.

  • Performance Comparison of Distributed Injection Methods for Hypersonic Film-Cooling

    Basore, K. D., Selzer, M., Wheatley, V., Boyce, R. R., Mee, D. J., Capra, B. R., Kuhn, M. and Brieschenk, S. (2016). Performance Comparison of Distributed Injection Methods for Hypersonic Film-Cooling. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, 5-8 December 2016. Victoria, Australia: Australasian Fluid Mechanics Society.

  • Plasma flow simulation using the two-fluid model

    Bond, D. M., Wheatley, V. and Samtaney, R. (2016). Plasma flow simulation using the two-fluid model. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, 5-8 December 2016. Victoria, Australia: Australasian Fluid Mechanics Society.

  • Preliminary Investigation of Sound Generation in Scramjets

    Gibbons, N., Wheatley, V. and Doolan, C. (2016). Preliminary Investigation of Sound Generation in Scramjets. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, 5-8 December 2016. Victoria, Australia: Australasian Fluid Mechanics Society.

  • Characterisation of the cylindrical Riemann problem in magnetohydrodynamics

    Mostert, W., Wheatley, V. and Samtaney, R. (2015). Characterisation of the cylindrical Riemann problem in magnetohydrodynamics. International Symposium on Shock Waves (ISSW29), Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16838-8_1

  • Combustion regimes in inlet-fueled, low compression scramjets

    Gehre, Rolf M., Wheatley, Vincent and Boyce, Russell R. (2015). Combustion regimes in inlet-fueled, low compression scramjets. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3507

  • Fluorescence studies of jet mixing in a hypersonic flow

    Brieschenk, S., Gehre, R., Wheatley, V. and Boyce, R. (2015). Fluorescence studies of jet mixing in a hypersonic flow. International Symposium on Shock Waves (ISSW29), Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_98

  • Numerical investigation of the mixing process in inlet-fuelled scramjets

    Gehre, R. M., Peterson, D., Wheatley, V. and Boyce, R. R. (2015). Numerical investigation of the mixing process in inlet-fuelled scramjets. International Symposium on Shock Waves (ISSW29), Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16838-8_32

  • Simulation of laser-induced-plasma ignition in a hypersonic crossflow

    Gibbons, Nicholas, Gehre, Rolf, Brieschenk, Stefan and Wheatley, Vincent (2015). Simulation of laser-induced-plasma ignition in a hypersonic crossflow. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3622

  • Tailored fuel injection for performance enhancement in a Mach 12 scramjet engine

    Barth, James E., Wise, Dylan J., Wheatley, Vincent and Smart, Michael K. (2015). Tailored fuel injection for performance enhancement in a Mach 12 scramjet engine. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3614

  • The magnetohydrodynamic Richtmyer-Meshkov instability: the oblique field case

    Wheatley, V., Gehre, R. M., Samtaney, R. and Pullin, D. I. (2015). The magnetohydrodynamic Richtmyer-Meshkov instability: the oblique field case. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16838-8_50

  • Characterization of a spark ignition system for flameholding cavities

    Brieschenk, Stefan, Pontalier, Quentin, Duffaut, Alexandre, Denman, Zachary J., Veeraravagan, Anand, Wheatley, Vincent and Smart, Michael K. (2014). Characterization of a spark ignition system for flameholding cavities. 45th AIAA Plasmadynamics and Lasers Conference 2014, Atlanta, United States, 16-20 June 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2014-2242

  • Equivalent direct connect free-stream shock tunnel conditions for injection locations in an axisymmetric scramjet

    Basore, K., Wheatley, V., Boyce, R. R. and Starkey, R. (2014). Equivalent direct connect free-stream shock tunnel conditions for injection locations in an axisymmetric scramjet. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.

  • Experimental design of a cavity flameholder in a Mach 8 Shape-Transitioning Scramjet

    Denman, Zachary J., Brieschenk, Stefan, Veeraragavan, Anand, Wheatley, Vincent and Smart, Michael K. (2014). Experimental design of a cavity flameholder in a Mach 8 Shape-Transitioning Scramjet. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, United States, 16-20 June 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2014-2953

  • Influence of a seed magnetic field on the imploding cylindrical Richtmyer-Meshkov instability in magnetohydrodynamics

    Mostert, W., Wheatley, V., Samtaney, R. and Pullin, D. I. (2014). Influence of a seed magnetic field on the imploding cylindrical Richtmyer-Meshkov instability in magnetohydrodynamics. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.

  • Inlet fuel injection in a mach 12 shape-transitioning scramjet

    Barth, James E., Wheatley, Vincent and Smart, Michael K. (2014). Inlet fuel injection in a mach 12 shape-transitioning scramjet. 52nd AIAA Aerospace Sciences Meeting, National Harbor, MD, United States, 13-17 January 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2014-1159

  • Irregular shock refraction in magnetohydrodynamics

    Bilgi, P., Wheatley, V., Samtaney, R. and Barth, J. E. (2014). Irregular shock refraction in magnetohydrodynamics. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.

  • Tailored fuel injection within a Mach 12 shape transitioning scramjet

    Landsberg, W. O., Barth, J. E., Veeraragavan, A., Wheatley, V. and Smart, M. K. (2014). Tailored fuel injection within a Mach 12 shape transitioning scramjet. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.

  • A parametric study of oxygen enriched scramjet combustion

    Petty, David J., Wheatley, V. and Smart, M. K. (2012). A parametric study of oxygen enriched scramjet combustion. 11th Australian Space Science Conference, Canberra, Australia, 26 - 29 September 2011. Sydney, Australia: National Space Society of Australia.

  • Arbitrarily high-order BGK-Shakhov method for the simulation of micro-channel flows

    Bond, D. M., Wheatley, V., Macrossan, M. N. and Goldsworthy, M. (2012). Arbitrarily high-order BGK-Shakhov method for the simulation of micro-channel flows. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3 - 7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.

  • Comparison of discrete BGK-Shakhov System with DSMC

    Bond, D. M., Macrossan, M. N. and Wheatley, V. (2012). Comparison of discrete BGK-Shakhov System with DSMC. 28th International Symposium on Rarefied Gas Dynamics (RGD), Zaragoza Spain, 09-13 July 2012. College Park, MD, United States: American Institute of Physics. doi: 10.1063/1.4769540

  • Effects of ethylene combustion in a hypersonic turbulent boundary layer

    Barth, James E., Wheatley, Vincent and Smart, Michael K. (2012). Effects of ethylene combustion in a hypersonic turbulent boundary layer. 11th Australian Space Science Conference, Canberra, Australia, 26 - 29 September 2011. Sydney, Australia: National Space Society of Australia.

  • Flow physics inside a shape-transitioning scramjet engine

    Barth, James E., Wheatley, Vincent, Smart, Michael K., Petty, David J. and Basore, Kevin D. (2012). Flow physics inside a shape-transitioning scramjet engine. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24-28 September 2012. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-5888

  • Hybrid reynolds-averaged and large-eddy simulation of mixing in an axisymmetric scramjet

    Peterson, David M., Boyce, Russell R. and Wheatley, Vincent (2012). Hybrid reynolds-averaged and large-eddy simulation of mixing in an axisymmetric scramjet. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24-28 September 2012. Reston, VA, United States: American Institute for Aeronautics and Astronautics. doi: 10.2514/6.2012-5902

  • Hypersonic viscous drag reduction via multi-porthole injector arrays

    Pudsey, Adrian S., Boyce, Russell R. and Wheatley, Vincent (2012). Hypersonic viscous drag reduction via multi-porthole injector arrays. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24-28 September 2012. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-5934

  • Jet interaction in a hypersonic flow: a comparison between PLIF thermometry and computational simulation

    Brieschenk, Stefan, Gehre, Rolf M., Wheatley, Vincent, Boyce, Russell R., Kleine, Harald and O'Byrne, Sean (2012). Jet interaction in a hypersonic flow: a comparison between PLIF thermometry and computational simulation. 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012, Brisbane, QLD, Australia, 23-28 September 2012. Stockholm, Sweden: International Council of The Aeronautical Sciences.

  • Jet interaction in a hypersonic flow: a comparison between plif thermometry and computational simulation

    Brieschenk, Stefan, Gehre, Rolf M., Wheatley, Vincent, Boyce, Russell R., Kleine, Harald and O’Byrne, Sean (2012). Jet interaction in a hypersonic flow: a comparison between plif thermometry and computational simulation. 28th International Congress of the Aeronautical Sciences (ICAS 2012), Brisbane, Australia, 23 - 28 September 2012. United Kingdom: International Council of the Aeronautical Sciences (ICAS).

  • Reynolds-averaged Navier–Stokes and wall–modelled large–eddy simulations of sonic hydrogen injection into hypersonic crossflow

    Gehre, R. M., Wheatley, V., Boyce, R. R., Peterson, D. M. and Brieschenk, S. (2012). Reynolds-averaged Navier–Stokes and wall–modelled large–eddy simulations of sonic hydrogen injection into hypersonic crossflow. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3-7 December, 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.

  • Streamwise porthole fuel injection for boundary-layer combustion inside a scramjet engine

    Barth, James E., Wheatley, Vincent and Smart, Michael K. (2012). Streamwise porthole fuel injection for boundary-layer combustion inside a scramjet engine. 28th International Congress of the Aeronautical Sciences (ICAS 2012), Brisbane, Australia, 23 - 28 September 2012. United Kingdom: International Council of the Aeronautical Sciences (ICAS).

  • The Cylindrical Riemann Problem in magnetohydrodynamics: a case study

    Mostert, W., Wheatley, V., Hingee, M. and Samtaney, R. (2012). The Cylindrical Riemann Problem in magnetohydrodynamics: a case study. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3-7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.

  • The magnetohydrodynamic Richtmyer-Meshkov instability: the transverse field case

    Wheatley, V., Samtaney, R. and Pullin, D. I. (2012). The magnetohydrodynamic Richtmyer-Meshkov instability: the transverse field case. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3 - 7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.

  • Thermal non-equilibrium effects in radical farming scramjets

    Gehre, Rolf M., Wheatley, Vincent and Boyce, Russell R. (2012). Thermal non-equilibrium effects in radical farming scramjets. Congress of the International Council of the Aeronautical Sciences, Brisbane, QLD, Australia, 23 - 28 September 2012. ICAS Secretariat.

  • Thermal non-equilibrium effects in radical farming scramjets

    Gehre, Rolf M., Wheatley, Vincent and Boyce, Russell R. (2012). Thermal non-equilibrium effects in radical farming scramjets. 28th International Congress of the Aeronautical Sciences (ICAS 2012), Brisbane, Australia, 23 - 28 September 2012. United Kingdom: International Council of the Aeronautical Sciences (ICAS).

  • Aeolian tones generated by a square cylinder with a detached flat plate

    Ali, Mohamed Sukri Mat Ali, Doolan, Con J. and Wheatley, Vincent (2011). Aeolian tones generated by a square cylinder with a detached flat plate. 17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), Portland, OR, United States, 5-8 June 2011. Reston, VA, United States: AIAA - American Institute of Aeronautics and Astronautics.

  • Hypersonic inlet for a laser powered propulsion system

    Harrland, Alan, Doolan, Con, Wheatley, Vincent and Froning, Dave (2011). Hypersonic inlet for a laser powered propulsion system. 7th International Symposium on Beamed Energy Propulsion, Ludwigsburg, Germany, 10 -14 April 2011. College Park, MD, United States: American Institute of Physics. doi: 10.1063/1.3657023

  • Spectral Performance of RKDG methods for Ideal MHD

    Wheatley, V., Kumar, H. and Jeltsch, R. (2011). Spectral Performance of RKDG methods for Ideal MHD. Mathematics in Industry 2010, Sofia, Bulgaria, 11-13 July 2010. Sofia, Bulgaria: Bulgarska Akademiya na Naukite * Institute of Mathematics and Informatics.

  • Aeolian tones generated by a square cylinder with a splitter plate

    Ali, Mohamed Sukri Mat, Doolan, Con J. and Wheatley, Vincent (2010). Aeolian tones generated by a square cylinder with a splitter plate.

  • Aeolian tones generated by a square cylinder with a splitter plate

    Ali, Mohamed Sukri Mat, Doolan, Con J. and Wheatley, Vincent (2010). Aeolian tones generated by a square cylinder with a splitter plate. 20th International Congress on Acoustics, Sydney, NSW, Australia, 23-27 August 2010. NSW, Australia: Australian Acoustical Society.

  • Flow around a square cylinder with a detached downstream flat plate at a low Reynolds number

    Ali, Mohamed Sukri Mat, Doolan, Con J. and Wheatley, Vincent (2010). Flow around a square cylinder with a detached downstream flat plate at a low Reynolds number. 17th Australasian Fluid Mechanics Conference, Auckland, New Zealand, 5-9 December 2010. Aukland, New Zealand: University of Auckland, Deptartment of Mechanical Engineering.

  • Fuel injection via rectangular cross-section injectors for mixing enhancement in scramjets

    Wheatley, V. and Jacobs, P. A. (2010). Fuel injection via rectangular cross-section injectors for mixing enhancement in scramjets. 17th Australasian Fluid Mechanics Conference, Auckland, New Zealand, 5-9 December 2010. Auckland, New Zealand: The University of Auckland.

  • Hypersonic inlet for a laser powered propulsion system and its interaction with an idealized laser induced detonation wave

    Harrland, Alan, Doolan, Con and Wheatley, Vincent (2010). Hypersonic inlet for a laser powered propulsion system and its interaction with an idealized laser induced detonation wave. 10th Australian Space Sciences Conference, Brisbane, Australia, 27-30 September 2010. Sydney, Australia: National Space Society of Australia.

  • Simulation of hypervelocity scramjet combustion with oxygen enrichment

    Petty, D., Smart, M. K., Wheatley, V. and Razzaqi, S. A. (2010). Simulation of hypervelocity scramjet combustion with oxygen enrichment. 10th Australian Space Sciences Conference, Brisbane, Australia, 27-30 September 2010. Sydney, Australia: National Space Society of Australia.

  • Grid convergence study for a two-dimensional simulation of flow around a square cylinder at low Reynolds number

    Ali, Mohamed Sukri Mat, Doolan, Con J. and Wheatley, Vincent (2009). Grid convergence study for a two-dimensional simulation of flow around a square cylinder at low Reynolds number. The 7th International Conference on CFD in the Minerals and Process Industries, Melbourne , Australia, 9-11 December, 2009. Melbourne, Vic., Australia: CSIRO.

  • Hypersonic Vehicle Control Using External Burning

    Doolan, C.J. and Vincent Wheatley (2009). Hypersonic Vehicle Control Using External Burning. Australian Combustion Symposium, University of Queensland Brisbane, Dec 2 -4, 2009. Brisbane :The University of Queensland.

  • Numerical simulation of compressible magnetohydrodynamic plasma flow in a circuit breaker

    Hiptmair, R., Hugueniot, P., Jeltsch, R., Kumar, H., Schwab, C., Torrilhon, M. and Wheatley, V. (2008). Numerical simulation of compressible magnetohydrodynamic plasma flow in a circuit breaker. International Conference on Numerical Analysis and Applied Mathematics, Psalidi, Greece, 16-20 September 2008. College Park, MD, United States: Springer New York LLC. doi: 10.1063/1.2990896

  • Numerical simulations of high current arc in circuit breakers

    Huguenot, P., Kumar, H., Wheatley, V., Jeltsch, R. and Schwab, C. (2008). Numerical simulations of high current arc in circuit breakers. 24th International Conference on Electrical Contacts, Saint-Malo, France, 9-12 June 2008.

  • Promotion of open and efficient communication in tutorials

    Mattner, Trent and Wheatley, Vincent (2008). Promotion of open and efficient communication in tutorials. Education Research Group of Adelaide 2008 Conference, Adelaide, SA, Australia, 24-25 September 2008. Adelaide, SA, Australia: The University of Adelaide.

Other Outputs

Grants (Administered at UQ)

PhD and MPhil Supervision

Current Supervision

  • Investigation of flow field manipulation, thermal compression and mode transition in a Mach 5-10 scramjet accelerator

    Doctor Philosophy — Principal Advisor

    Other advisors:

  • Two-fluid modeling of electron transpiration cooling for the leading edges of hypersonic vehicles

    Doctor Philosophy — Principal Advisor

    Other advisors:

  • Experimental Investigation of Hypersonic Boundary Layer Combustion of Hydrocarbon Fuels

    Doctor Philosophy — Principal Advisor

    Other advisors:

  • Computational Investigation of Sound Generation and Propagation in Scramjet Engines

    Doctor Philosophy — Principal Advisor

    Other advisors:

  • Investigation of electron behavior, instabilities, and suppression mechanisms in RMI and RTI affected inertial confinement fusion

    Doctor Philosophy — Principal Advisor

    Other advisors:

  • Investigation into Electron Transpiration Cooling in Hypersonic Flow Conditions

    Doctor Philosophy — Associate Advisor

    Other advisors:

  • Examining Growth of Turbulence Over Heated Walls in Hypersonic Flows

    Doctor Philosophy — Associate Advisor

    Other advisors:

  • Concentrated breakdown in boundary layer transition in a hypersonic flow

    Master Philosophy — Associate Advisor

    Other advisors:

  • Experimental investigation of scramjet acoustic loads

    Doctor Philosophy — Associate Advisor

    Other advisors:

  • Advanced Biodegradable Materials: Functionally graded, crystalline plus amorphous Mg alloys produced by laser metal deposition and laser surface modification

    Doctor Philosophy — Associate Advisor

    Other advisors:

  • Mars atmosphere magnetohydrodynamic aerobraking

    Doctor Philosophy — Associate Advisor

    Other advisors:

Completed Supervision

Possible Research Projects

Note for students: The possible research projects listed on this page may not be comprehensive or up to date. Always feel free to contact the staff for more information, and also with your own research ideas.

  • Numerical investigation of scramjet acoustic loads

    Acoustic loads in hypersonic air-breathing engines have been recognized as a serious issue since the 1980s, yet their mitigation remains an open problem. With the successful X51 flight tests at low hypersonic Mach numbers and our success in the laboratory at up to Mach 12, resolving the remaining technical barriers to developing reusable hypersonic vehicles has gained immediate importance. The first step towards effective mitigation or management of scramjet acoustic loads is to develop the capability to accurately predict and understand them. It is this important problem that the proposed research aims to address as part of the 2017 ARC Discovery Project “Acoustic loads on hypersonic vehicles”.

    The primary goal of this PhD project is to conduct Wall-Modelled Large-Eddy Simulation (WMLES) of the supersonic and hypersonic experiments conducted by other students, then through comparison of the numerical and experimental acoustic data, refine the simulation approach and ultimately validate it. Once the simulation approach has been validated, WMLES will provide highly detailed, time accurate data upon which to build our understanding of the sound generation mechanisms in scramjets. The approach will also be able to accurately predict the acoustic loads in other supersonic engines.

  • Two-fluid MHD investigation of the magnetic suppression of shock driven plasma instabilities

    In inertial confinement fusion, hundreds of terawatts of laser power is used to drive a converging shock wave into a small spherical capsule containing a fuel mixture of heavy hydrogen isotopes. When the shock wave converges at the centre of the capsule, the temperature should exceed 100 million Kelvin and a fusion reaction between the hydrogen nuclei should be ignite. The fusion burn should then propagate outward through the fuel more rapidly than it can expand. However, when the shock impacts on the interfaces between the capsule and the fuel layers, hydrodynamic instabilities are triggered. The first of these is the Richtmyer-Meshkov instability, which occurs when a shock interacts with a density interface. The hydrodynamic instabilities limit the chance of energy break-even or production.

    In the last few years, we have shown that in ideal plasmas, the Richtmyer-Meshkov instability can be suppressed by the application of a seed magnetic field. The extreme temperatures involved in inertial confinement fusion mean the fluids involved are plasmas, so suppressing the instability is possible. Unfortunately, to suppress the instability and maintain spherical symmetry would require a radial magnetic field, which is not attainable. Instead we have studied cases where the instability is suppressed using realistic magnetic fields, with very promising results.

    The results discussed above were obtained using ideal magnetohydrodynamics (MHD), which is one of the simplest frameworks for modelling plasma behaviour. In this project, the suppression of the Richtmyer-Meskov instability will be investigated using the more realistic framework of two-fluid MHD, where the electrons and heavy ions are simulated separately, and the full set of Maxwell's equations are solved to determine the evolution of the electric and magnetic fields. This framework allows a wealth of plasma behaviour that cannot occur in ideal MHD. The crucial outcome of this project will be to determine how these phenomena affect the suppression of the Ritchmyer-Meshkov instability in the presence of a seed magnetic field.

  • Experimental investigation of scramjet acoustic loads

    Acoustic loads in hypersonic air-breathing engines have been recognized as a serious issue since the 1980s, yet their mitigation remains an open problem. With the successful X51 flight tests at low hypersonic Mach numbers and our success in the laboratory at up to Mach 12, resolving the remaining technical barriers to developing reusable hypersonic vehicles has gained immediate importance. An essential step towards effective mitigation or management of scramjet acoustic loads is to measure them in a realistic environment, providing vital data to validate predictive models. It is this important problem that the proposed research aims to address as part of the 2017 ARC Discovery Project “Acoustic loads on hypersonic vehicles”.

    The primary goal of this PhD project is experimentally measure acoustic loads in a scramjet engine under realistic hypersonic flight and fuel injection conditions in UQ’s T4 Shock Tunnel. This facility can faithfully recreate the flow physics in scramjet engines, including the acoustic environment. The experimental measurement of acoustic waves in shock tunnels is extremely challenging: The impact of the free-piston driver, diaphragm bursting and transient shock reflections produce intense structural vibrations. Test flows at multiple kilometers per second are generated with stagnation temperatures of over 5000 K. Many of the sensors typically used in aeroacoustics cannot withstand this extreme thermal environment. We will overcome these limitations and resolve all waves above 5 kHz by using the focused laser differential interferometer (FLDI) technique. This method has been proven to work in the T5 shock tunnel in Caltech for external flows; this will be the first application to scramjet flows in a reflected shock tunnel. The method will be extended to simultaneously measure perturbations at three locations, enabling acoustic signals to be distinguished from entropy waves. The proposed experimental design will produce a supersonic turbulent reacting flow with features that closely match those in a candidate access-to-space scramjet. Using FLDI to probe the sound field at key points will permit a high-fidelity, time-resolved comparison between experimental and numerical data for validation purposes.

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ResearcherID: D-9627-2013

ORCID: 0000-0002-7287-7659

Scopus ID: 8984492900

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