Skip to menu Skip to content Skip to footer
Associate Professor Rowan Gollan
Associate Professor

Rowan Gollan

Email: 
Phone: 
+61 7 336 53851

Overview

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

Associate Professor Rowan Gollan is:
Available for supervision

Qualifications

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

Works

Search Professor Rowan Gollan’s works on UQ eSpace

107 works between 2001 and 2025

81 - 100 of 107 works

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

2010

Conference Publication

Design of modular shape-transitioning inlets for a conical hypersonic vehicle

Gollan, Rowan J. and Smart, Michael K. (2010). Design of modular shape-transitioning inlets for a conical hypersonic vehicle. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, United States, 4-7 January 2010. Red Hook, NY, United States: Curran Associates. doi: 10.2514/6.2010-940

Design of modular shape-transitioning inlets for a conical hypersonic vehicle

2010

Conference Publication

Adaption and use of a compressible flow code for turbomachinery design

Ventura, Carlos, Sauret, Emilie, Jacobs, Peter, Petrie-Repar, Paul, Gollan, Rowan and Van Der Laan, Paul (2010). Adaption and use of a compressible flow code for turbomachinery design. V European Conference on Computational Fluid Dynamics ECCOMAS CFD, Lisbon, Portugal, 14-17 June 2010.

Adaption and use of a compressible flow code for turbomachinery design

2010

Conference Publication

CFD Tools for Design and Simulation of Transient Flows in Hypersonic Facilities

Jacobs, P. A., Gollan, R. J., Potter, D. F., Gildfind, D. E., Eichmann, T. N., O'Flaherty, B. F. and Buttsworth, D. R. (2010). CFD Tools for Design and Simulation of Transient Flows in Hypersonic Facilities. AVT-186 RTO AVT/VKI Lecture Series - Aerothermodynamic design, review on ground testing and CFD, Genese, Belgium, 29 March-01 April 2010. Genese, Belgium: von Karman Institute.

CFD Tools for Design and Simulation of Transient Flows in Hypersonic Facilities

2009

Journal Article

Helmholtz Resonance of Pitot Pressure Measurements in Impulsive Hypersonic Test Facilities

McGilvray, M., Jacobs, P.A., Morgan, R.G., Gollan, R.J. and Jacobs, C.M. (2009). Helmholtz Resonance of Pitot Pressure Measurements in Impulsive Hypersonic Test Facilities. AIAA Journal, 47 (10), 2430-2439. doi: 10.2514/1.42543

Helmholtz Resonance of Pitot Pressure Measurements in Impulsive Hypersonic Test Facilities

2009

Conference Publication

A simulation technique for radiating shock tube flows

Rowan Gollan, Carolyn Jacobs, Jacobs, Peter A., Morgan, Richard G., McIntyre, Timothy J., Macrossan, Michael N., Buttsworth, David R., Eichmann, Troy N. and Daniel Potter (2009). A simulation technique for radiating shock tube flows. 26th International Symposium on Shock Waves (ISSW26), Gottingen, Germany, 15-20 July. Berlin, Germany: Springer-Verlag Heidelberg. doi: 10.1007/978-3-540-85168-4_74

A simulation technique for radiating shock tube flows

2009

Conference Publication

Numerical simulations and analysis of the 8.5 km/s CO2-N2 east shock tube condition

Potter, D. F., Gollan, R. J., Jacobs, P. A. and Leyland, P. (2009). Numerical simulations and analysis of the 8.5 km/s CO2-N2 east shock tube condition. 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Heraklion, Greece, 30 September - 3 October 2008. Noordwijk, The Netherlands: ESA Communication Production Office.

Numerical simulations and analysis of the 8.5 km/s CO2-N2 east shock tube condition

2008

Other Outputs

Computational modelling of high-temperature gas effects with application to hypersonic flows

Gollan, Rowan (2008). Computational modelling of high-temperature gas effects with application to hypersonic flows. PhD Thesis, School of Engineering, The University of Queensland. doi: 10.14264/178818

Computational modelling of high-temperature gas effects with application to hypersonic flows

2008

Conference Publication

Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers

Potter, Daniel F., Gollan, Rowan J., Eichmann, Troy, McIntyre, Tim J., Morgan, Richard G. and Jacobs, Peter A. (2008). Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers. 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 7-10 january 2008.

Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers

2008

Conference Publication

Impulse facilities for the simulation of hypersonic radiating flows

Morgan, R. G., McIntyre, T. J., Buttsworth, D. R., Jacobs, P. A., Potter, D. F., Brandis, A. M., Gollan, R. J., Jacobs, C. M., Capra, B. R., McGilvray, M. and Eichmann, T. (2008). Impulse facilities for the simulation of hypersonic radiating flows. 38th Fluid Dynamics Conference and Exhibit, Seattle, Washington, U.S.A., 23 - 26 June, 2008. Reston, VA, U.S.A.: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2008-4270

Impulse facilities for the simulation of hypersonic radiating flows

2007

Conference Publication

Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers

Potter, D. F., Gollan, R. J., Eichmann, T., Jacobs, P. A., Morgan, R. G. and McIntyre, T. J. (2007). Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Queensland: School of Engineering, The University of Queensland.

Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers

2007

Conference Publication

Development of Casbar: a Two-phase Flow Code for the Interior Ballistics Problem

Gollan, R. J., Johnston, I. A., O’Flaherty, B. T. and Jacobs, P. A. (2007). Development of Casbar: a Two-phase Flow Code for the Interior Ballistics Problem. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 2-7 December 2007. Brisbane, Australia: School of Engineering, The University of Queensland.

Development of Casbar: a Two-phase Flow Code for the Interior Ballistics Problem

2006

Conference Publication

Analytical maps of aerodynamic damping as a function of operating condition for a compressor profile

Petrie-Repar, Paul J., McGhee, Andrew, Jacobs, Peter A. and Gollan, Rowan (2006). Analytical maps of aerodynamic damping as a function of operating condition for a compressor profile. TE06: ASME Turbo Expo 2006, Barcelona, Spain, 8-11 May 2006. New York, NY, U.S.A.: ASME. doi: 10.1115/GT2006-90829

Analytical maps of aerodynamic damping as a function of operating condition for a compressor profile

2006

Conference Publication

Radiation measurements in nonreflected shock tunnels

Morgan, Richard, McIntyre, Tim, Gollan, Rowan, Jacobs, Peter, Brandis, Aaron, McGilvray, Matthew, van Diem, Dwight, Gnoffo, Peter, Pulsonnetti, Maria and Wright, Michael (2006). Radiation measurements in nonreflected shock tunnels. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, California, USA, 5-8 June 2006. Reston, VA, U.S.A.: American Institute of Aeronautics and Astronautics.

Radiation measurements in nonreflected shock tunnels

2006

Conference Publication

Impulse facility simulation of hypervelocity radiating flows

Brandis, A. M., Buttsworth, D. R., Capra, B. R., Eichmann, T., Gollan, R. J., Jacobs, C. M., Jacobs, P. A., Macrossan, M. N., McGilvray, M., McIntyre, T. J., Morgan, R. G., Potter, D. F., Scott, M. P. and van Diem, D. (2006). Impulse facility simulation of hypervelocity radiating flows. 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Rome, Italy, 6-8 September 2006. The Netherlands: ESA Publications.

Impulse facility simulation of hypervelocity radiating flows

Funding

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

Past funding

  • 2023
    Aerodynamic characterisation of textured fabrics
    AusCycling Pty Ltd
    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
  • 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

Supervision

Availability

Associate Professor Rowan Gollan is:
Available for supervision

Before you email them, read our advice on how to contact a supervisor.

Supervision history

Current supervision

  • 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

    Numerical modelling of electron transpiration cooling for hypersonic vehicles

    Principal Advisor

    Other advisors: Dr Nick Gibbons

  • 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

    Tailoring surface conditions to control transition in hypersonic boundary layers

    Principal Advisor

    Other advisors: Dr Nick Gibbons

  • Doctor Philosophy

    Shape Morphing Hypersonic Vehicles

    Principal Advisor

    Other advisors: Professor Vincent Wheatley

  • Doctor Philosophy

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

    Principal Advisor

  • Doctor Philosophy

    State-to-state modelling of nonequilibrium reacting shock layers

    Principal Advisor

    Other advisors: Dr Carolyn Jacobs, Dr Nick Gibbons

  • Doctor Philosophy

    Numerical modelling of electron transpiration cooling for hypersonic vehicles

    Principal Advisor

    Other advisors: Dr Nick Gibbons

  • 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

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

    Principal Advisor

  • Doctor Philosophy

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

    Principal Advisor

  • Doctor Philosophy

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

    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

  • 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

  • Doctor Philosophy

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

    Associate Advisor

    Other advisors: Professor Vincent Wheatley

Completed supervision

Media

Enquiries

For media enquiries about Associate Professor Rowan Gollan's areas of expertise, story ideas and help finding experts, contact our Media team:

communications@uq.edu.au