Dr Rowan Gollan
Dr

Rowan Gollan

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Phone: 
+61 7 336 53851

Background

Dr Rowan Gollan was awarded his PhD in the field of Aerospace Engineering from UQ in 2009, where he was awarded the 2010 John Simmons Prize for best thesis in the School of Mechanical and Mining Engineering and The University of Queensland Dean’s Award for Outstanding Research Higher Degree Thesis. From August 2008, while his thesis was under examination, Rowan took up a position as a research scientist at the NASA Langley Research Center in the United States, working in the Hypersonic Airbreathing Propulsion Branch. Rowan returned to UQ in January 2012 in a position funded by the Defence Science & Technology Organisation (DSTO). In his role as an aerodynamic analyst, Rowan uses state-of-the-art hypersonic analysis techniques to simulate an experimental flight vehicle.

Dr Gollan was awarded an Australian Research Council (ARC) Discovery Early Career Researcher Award (DECRA), which he commenced in 2014.

DECRA Project summary: Next-generation launch vehicles using high-speed jet engines will make it cheaper and more reliable for humankind to engage in activities in space. This project will contribute to the technology of high-speed jet engines by developing optimised air intake systems. The research aims to advance the use of computational engineering and apply this to improve the design of air intake systems.The outcomes of this project will advance the technology of high-speed jet engines with the goal of replacing existing rocket systems.

Availability

Dr Rowan Gollan is:
Available for supervision

Qualifications

  • Bachelor (Honours) of Engineering, The University of Queensland
  • Doctor of Philosophy, The University of Queensland

Search Professor Rowan Gollan’s works on UQ eSpace

101 works between 2001 and 2024
All (101) Journal Article (32) Conference Publication (63) Other Outputs (6)

61 - 80 of 101 works

2016

Conference Publication

Verification of the least-squares procedure within an unstructured-grid flow solver

Damm, K. A., Gollan, R. J. and Jacobs, P. A. (2016). Verification of the least-squares procedure within an unstructured-grid flow solver. 20th Australasian Fluid Mechanics Conference, Perth, Australia, 5-8 December 2016. Australasian Fluid Mechanics Society.

Verification of the least-squares procedure within an unstructured-grid flow solver

2016

Conference Publication

Verification of RANS turbulence model in Eilmer using the Method of Manufactured Solutions

Wang, J., Gollan, R. J. and Veeraragavan, A. (2016). Verification of RANS turbulence model in Eilmer using the Method of Manufactured Solutions. 20th Australasian Fluid Mechanics Conference, Perth, Australia, 5 – 8 December 2016. Perth, Australia: Australasian Fluid Mechanics Society.

Verification of RANS turbulence model in Eilmer using the Method of Manufactured Solutions

2016

Conference Publication

On the effect of outflow boundary truncation for numerical simulation of narrow-channel flames

Kang, X., Gollan, R. J., Jacobs, P. A. and Veeraragavan, A . (2016). On the effect of outflow boundary truncation for numerical simulation of narrow-channel flames. 20th Australasian Fluid Mechanics Conference, Perth, Australia, 5 – 8 December 2016. Perth, Australia: Australasian Fluid Mechanics Society.

On the effect of outflow boundary truncation for numerical simulation of narrow-channel flames

2015

Conference Publication

Shock standoff on hemi-spherical bodies in hypervelocity flows

Zander, F., Jacobs, P. A., Gollan, R. J. and Morgan, R. G. (2015). Shock standoff on hemi-spherical bodies in hypervelocity flows. 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_85

Shock standoff on hemi-spherical bodies in hypervelocity flows

2015

Conference Publication

Acceleration of combustion simulations using GPUs

Damm, K. A., Gollan, R. J. and Veeraragavan, A. (2015). Acceleration of combustion simulations using GPUs. Australian Combustion Symposium, Parkville, VIC, Australia, 7-9 December 2015. Melbourne, VIC, Australia: Combustion Institute Australian and New Zealand Section.

Acceleration of combustion simulations using GPUs

2015

Conference Publication

Effect of Streamwise Vortices on Scramjets Porthole Injection Mixing

Gomez, Juan Ramon Llobet, Jahn, Ingo H. and Gollan, Rowan (2015). Effect of Streamwise Vortices on Scramjets Porthole Injection Mixing. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July 2015. Reston, VA United States: AIAA. doi: 10.2514/6.2015-3597

Effect of Streamwise Vortices on Scramjets Porthole Injection Mixing

2015

Conference Publication

Numerical simulation of premixed methane/air flame dynamics in narrow channels

Kang, X., Gollan, R. J., Jacobs, P. A. and Veeraragavan, A. (2015). Numerical simulation of premixed methane/air flame dynamics in narrow channels. Australian Combustion Symposium, Parkville, VIC, Australia, 7-9 December 2015. Melbourne, VIC, Australia: Combustion Institute Australian and New Zealand Section.

Numerical simulation of premixed methane/air flame dynamics in narrow channels

2015

Conference Publication

Implementation of a compressible-flow simulation code in the D programming language

Jacobs, Peter and Gollan, Rowan (2015). Implementation of a compressible-flow simulation code in the D programming language. Australasian Conference on Computational Mechanics, Brisbane, Australia, 30 November to 1 December 2015.

Implementation of a compressible-flow simulation code in the D programming language

2014

Journal Article

Hypervelocity shock standoff on spheres in air

Zander, F., Gollan, R. J., Jacobs, P. A. and Morgan, R. G. (2014). Hypervelocity shock standoff on spheres in air. Shock Waves, 24 (2), 171-178. doi: 10.1007/s00193-013-0488-x

Hypervelocity shock standoff on spheres in air

2014

Other Outputs

Estimation of high-enthalpy flow conditions for simple shock and expansion processes using the ESTCj program and library

Jacobs, P. A., Gollan, R. J., Potter, D. F., Zander, F., Gildfind, D. E., Blyton, P., Chan, W. Y. K. and Doherty, L. (2014). Estimation of high-enthalpy flow conditions for simple shock and expansion processes using the ESTCj program and library. Mechanical Engineering Report 2011/02 St Lucia, QLD, Australia:

Estimation of high-enthalpy flow conditions for simple shock and expansion processes using the ESTCj program and library

2014

Conference Publication

Numerical simulations of premixed combustion in narrow channels

Kang, X ., Gollan, R . J., Jacobs, P . A. and Veeraragavan, A . (2014). Numerical simulations of premixed combustion in narrow channels. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.

Numerical simulations of premixed combustion in narrow channels

2013

Journal Article

About the formulation, verification and validation of the hypersonic flow solver Eilmer

Gollan, R. J. and Jacobs, P. A. (2013). About the formulation, verification and validation of the hypersonic flow solver Eilmer. International Journal for Numerical Methods in Fluids, 73 (1), 19-57. doi: 10.1002/fld.3790

About the formulation, verification and validation of the hypersonic flow solver Eilmer

2013

Journal Article

Design of Modular Shape-Transition Inlets for a Conical Hypersonic Vehicle

Gollan, Rowan J. and Smart, Michael K. (2013). Design of Modular Shape-Transition Inlets for a Conical Hypersonic Vehicle. Journal of Propulsion and Power, 29 (4), 832-838. doi: 10.2514/1.B34672

Design of Modular Shape-Transition Inlets for a Conical Hypersonic Vehicle

2013

Conference Publication

Design, operation and testing in expansion tube facilities for super-orbital re-entry

Jacobs, Peter, Morgan, Richard, Brandis, Aaron, Buttsworth, David, Dann, Andrew, D'Souza, Mary, Eichmann, Troy, Gildfind, David, Gollan, Rowan, Jacobs, Carolyn, McGilvray, Matthew, McIntyre, Tim, Mudford, Neil, Porat, Hadas, Potter, Dan and Zander, Fabian (2013). Design, operation and testing in expansion tube facilities for super-orbital re-entry. STO-AVT-VKI Lecture Series Radiation and Gas-Surface Interaction Phenomena in High Speed Re-Entry (2013-AVT-218), Rhode-St-Genèse, Belgium, 6-8 May 2013.

Design, operation and testing in expansion tube facilities for super-orbital re-entry

2012

Other Outputs

The compressible-flow CFD project

Jacobs, Peter A., Gollan, Rowan J. and Potter, Daniel F. (2012). The compressible-flow CFD project. Brisbane, QLD, Australia: The University of Queensland, School of Mechanical and Mining Engineering.

The compressible-flow CFD project

2012

Conference Publication

On the validation of a hypersonic flow solver using measurements of shock detachment distance

Gollan, Rowan J. and Jacobs, Peter A. (2012). On the validation of a hypersonic flow solver using measurements of shock detachment distance. International Symposium on Shock Waves (28th, ISSW28), Manchester, U.K., 17-22 July 2011. Heidelberg, Germany: Springer.

On the validation of a hypersonic flow solver using measurements of shock detachment distance

2012

Conference Publication

Mach disk platform for studying radiating flows

Zander, Fabian, Morgan, Richard G., Molder, Sannu, Jacobs, Peter A., Gollan, Rowan, Porat, Hadas and McIntyre, Timothy J. (2012). Mach disk platform for studying radiating flows. 5th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Barcelona, Spain, 16-19 October 2012. Noordwijk, The Netherlands : ESA Communications .

Mach disk platform for studying radiating flows

2012

Conference Publication

Verification of a compressible flow solver

Gollan, R. J. and Jacobs, P. A. (2012). Verification of a compressible flow solver. 18th Australasian Fluid Mechanics Conference (AFMC), Launceston, Australia, 3-7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.

Verification of a compressible flow solver

2012

Conference Publication

High temperature gas effects for converging conical shocks

Zander, F., Molder, S., Morgan, R. G., Jacobs, P. A. and Gollan, R. J. (2012). High temperature gas effects for converging conical shocks. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, 24 - 28 September 2012. Red Hook, N.Y: Currans. doi: 10.2514/6.2012-5939

High temperature gas effects for converging conical shocks

2011

Conference Publication

Investigation of REST-class hypersonic inlet designs

Gollan, Rowan J. and Ferlemann, Paul G. (2011). Investigation of REST-class hypersonic inlet designs. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011, San Francisco, CA United States, 11-14 April 2011. Reston, VA United States: AIAA. doi: 10.2514/6.2011-2254

Investigation of REST-class hypersonic inlet designs

Current funding

  • 2024 - 2025
    Ground testing and trajectory simulations of the BOLT 1b Hypersonic Boundary Layer Transition Flight Experiment
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2024 - 2025
    Characterisation and Modelling of Ablative Material Performance (DSP Research Agreement)
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2023 - 2025
    Investigating the Influence of Tailored Wall Temperature Profiling on Hypersonic Boundary Layer Transition
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2022 - 2025
    Dispersion of spacecraft components during re-entry (ARC Discovery Project administered by Uni of Southern Qld)
    University of Southern Queensland
    Open grant
  • 2022 - 2025
    Tuning parallel applications on software-defined supercomputers
    ARC Linkage Projects
    Open grant
  • 2022 - 2024
    Combustion-Driven HEL Technology Platform
    University of New South Wales
    Open grant

Past funding

  • 2023
    Aerodynamic characterisation of textured fabrics
    AusCycling Pty Ltd
    Open grant
  • 2020 - 2024
    Advanced Ground Testing and Simulation of the Boundary Layer Transition (BOLT) Flight Experiment
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2020 - 2023
    Non-equilibrium reacting shock layers
    ARC Discovery Projects
    Open grant
  • 2019 - 2023
    Electron Transpiration Cooling of Hypersonic Vehicles
    ARC Linkage Projects
    Open grant
  • 2019 - 2022
    Study of Non-Equilibrium Wakes Model
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2018
    Functional Representation of Generic Surfaces for CFD Applications
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2017 - 2019
    Experimental Studies of High-Speed Flows
    National University of Singapore Research Collaboration Agreement
    Open grant
  • 2017 - 2019
    High power density motors incorporating advanced manufacturing methods (CRC - Project led by MagniX)
    Cooperative Research Centre Projects
    Open grant
  • 2017 - 2019
    Turbulent heat transfer during Mars Venus and Earth atmospheric entry
    ARC Discovery Projects
    Open grant
  • 2016 - 2019
    Rapidly expanding non equilibrium hypersonic flow
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2014 - 2017
    Development of computer-based optimisation to improve hypersonic aerodynamic design.
    ARC Discovery Early Career Researcher Award
    Open grant
  • 2014
    A parallel computer facility for modelling and simulation
    UQ Major Equipment and Infrastructure
    Open grant
  • 2006 - 2007
    Development of software and methods to simulate gun interior ballistics in accordance with the contract condiitions and statement of requirement.
    Department Defence - Defence Science & Technology
    Open grant

Availability

Dr Rowan Gollan is:
Available for supervision

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Supervision history

Current supervision

  • Doctor Philosophy

    Qualitative Study of Radial-Inflow Turbine Working with High-Dense Gases

    Principal Advisor

  • Doctor Philosophy

    Development of an entropic lattice Boltzmann model for compressible fluid-structure interaction

    Principal Advisor

    Other advisors: Dr Chris James, Dr Nick Gibbons

  • Doctor Philosophy

    State-to-state modelling of nonequilibrium reacting shock layers

    Principal Advisor

    Other advisors: Dr Carolyn Jacobs, Dr Nick Gibbons

  • Doctor Philosophy

    Adjoint-based Optimisation of an Integrated Forebody and Inlet for Hypersonic Flight

    Principal Advisor

  • Doctor Philosophy

    Shape Morphing Hypersonic Vehicles

    Principal Advisor

    Other advisors: Professor Vincent Wheatley

  • Doctor Philosophy

    Numerical modelling of electron transpiration cooling for hypersonic vehicles

    Principal Advisor

    Other advisors: Dr Nick Gibbons

  • Doctor Philosophy

    Design and Optimize Heat Exchanger for Super Critical CO2 Power Plant Cooling (25 MW)

    Principal Advisor

  • Doctor Philosophy

    Direct Numerical Simulation of High-Speed Flows using Graphics Processing Units

    Principal Advisor

  • Doctor Philosophy

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

    Associate Advisor

    Other advisors: Professor Vincent Wheatley

  • Doctor Philosophy

    Optimised use of Magnetohydrodynamic Aerobraking for Planetary Atmospheric Entry

    Associate Advisor

    Other advisors: Professor Vincent Wheatley, Dr David Gildfind

  • Doctor Philosophy

    Co-design of hypersonic vehicle shape and trajectory

    Associate Advisor

  • Doctor Philosophy

    On the Repeatability and Flow Characterisation of Hypersonic Ground Test Facilities

    Associate Advisor

    Other advisors: Professor Richard Morgan, Dr Carolyn Jacobs, Dr Chris James

Completed supervision

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