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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

41 - 60 of 107 works

2019

Journal Article

Characterisation of the eddy dissipation model for the analysis of hydrogen-fuelled scramjets

Hoste, J. J.O.E., Fossati, M., Taylor, I. J. and Gollan, R. J. (2019). Characterisation of the eddy dissipation model for the analysis of hydrogen-fuelled scramjets. Aeronautical Journal, 123 (1262), 536-565. doi: 10.1017/aer.2018.169

Characterisation of the eddy dissipation model for the analysis of hydrogen-fuelled scramjets

2019

Conference Publication

Design of experiments for expansion tube evaluation of magnetohydrodynamic aerobraking for Earth return from deep space

Lefevre, Alexis, Gildfind, David E., Gollan, Rowan J. and Jacobs, Peter A. (2019). Design of experiments for expansion tube evaluation of magnetohydrodynamic aerobraking for Earth return from deep space. 32nd International Symposium on Shock Waves, Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0207-cd

Design of experiments for expansion tube evaluation of magnetohydrodynamic aerobraking for Earth return from deep space

2019

Conference Publication

Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnel

Cullen, T. G., James, C. M., Gollan, R. J. and Morgan, R. G. (2019). Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnel. 31st International Symposium on Shock Waves, Nagoya, Japan, 9-14 July 2017. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-91017-8_24

Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnel

2019

Conference Publication

Vibrational state-to-state modeling of a recombining nitrogen/argon plasma

Mariotto, P., Tibère-Inglesse, A., McGuire, S., Perrin, M. Y., Laux, C. O., Jacobs, P. and Gollan, R. (2019). Vibrational state-to-state modeling of a recombining nitrogen/argon plasma. AIAA Scitech 2019 Forum, San Diego, CA, United States, 7-11 January 2019. Reston, VA, United States: American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/6.2019-0796

Vibrational state-to-state modeling of a recombining nitrogen/argon plasma

2019

Conference Publication

Application of Infrared Thermography in an Expansion Tunnel

Cullen, T., James, C., Gollan, R. and Morgan, R. (2019). Application of Infrared Thermography in an Expansion Tunnel. In: Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019). 32nd International Symposium on Shock Waves (ISSW32 2019), Singapore, (1139-1165). 14-19 July 2019. doi:10.3850/978-981-11-2730-4_0271-cd

Application of Infrared Thermography in an Expansion Tunnel

2018

Journal Article

Scramjet Performance with Nonuniform Flow and Swept Nozzles

Bricalli, Mathew G., Brown, Laurie, Boyce, Russell R., Gollan, Rowan, Vanyai, Tristan and Pudsey, Adrian S. (2018). Scramjet Performance with Nonuniform Flow and Swept Nozzles. AIAA Journal, 56 (10), 1-16. doi: 10.2514/1.j056963

Scramjet Performance with Nonuniform Flow and Swept Nozzles

2018

Conference Publication

A design method for elliptical to rectangular shape transition nozzles

Kunze, Jens, Smart, Michael K. and Gollan, Rowan (2018). A design method for elliptical to rectangular shape transition nozzles. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018, Orlando, FL, United States, September 17, 2018-September 19, 2018. Reston, VA, United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2018-5318

A design method for elliptical to rectangular shape transition nozzles

2018

Conference Publication

Two way coupled hypersonic fluid structure interaction simulations with Eilmer

Jahn, I. H. J., Currao, G. M. D., Neely, A. J., Gollan, R. and Jacobs, P. (2018). Two way coupled hypersonic fluid structure interaction simulations with Eilmer. 21st Australasian Fluid Mechanics Conference, Adelaide, SA, Australia, 10-13 December 2018. Australasian Fluid Mechanics Society.

Two way coupled hypersonic fluid structure interaction simulations with Eilmer

2018

Conference Publication

Development of a rapid inviscid-boundary layer aerodynamics tool

Ward, Alexander D. T., Smart, Michael K. and Gollan, Rowan J. (2018). Development of a rapid inviscid-boundary layer aerodynamics tool. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018, Orlando, FL, United States, September 17, 2018-September 19, 2018. Reston, VA, United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2018-5270

Development of a rapid inviscid-boundary layer aerodynamics tool

2018

Conference Publication

Flow characterization and modeling of the X2 and X3 expansion tubes

Gildfind, David E., Jacobs, Peter A., Gollan, Rowan J., Toniato, Pierpaolo, McIntyre, Timothy J., Andrianatos, Andreas, James, Christopher M. and Morgan, Richard G. (2018). Flow characterization and modeling of the X2 and X3 expansion tubes. VKI Lecture Series STO-AVT-235 on Flow Characterization and Modeling of Hypersonic Wind Tunnels, Brussels, Belgium, 3-5 December 2018.

Flow characterization and modeling of the X2 and X3 expansion tubes

2018

Conference Publication

Simulation of a rotating detonation ramjet model in Mach 4 flow

Zhao, Mengmeng, Buttsworth, David, Gollan, Rowan and Jacobs, Peter (2018). Simulation of a rotating detonation ramjet model in Mach 4 flow. 21st Australasian Fluid Mechanics Conference, Adelaide, SA Australia, 10-13 December 2018. Perth, WA Australia: Australasian Fluid Mechanics Society.

Simulation of a rotating detonation ramjet model in Mach 4 flow

2017

Journal Article

Scramjet test flow reconstruction for a large-scale expansion tube, Part 2: axisymmetric CFD analysis

Gildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. C. and Gollan, R. J. (2017). Scramjet test flow reconstruction for a large-scale expansion tube, Part 2: axisymmetric CFD analysis. Shock Waves, 28 (4), 1-20. doi: 10.1007/s00193-017-0786-9

Scramjet test flow reconstruction for a large-scale expansion tube, Part 2: axisymmetric CFD analysis

2017

Journal Article

Scramjet test flow reconstruction for a large-scale expansion tube, part 1: quasi-one-dimensional modelling

Gildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. K. and Gollan, R. J. (2017). Scramjet test flow reconstruction for a large-scale expansion tube, part 1: quasi-one-dimensional modelling. Shock Waves, 28 (4), 1-21. doi: 10.1007/s00193-017-0785-x

Scramjet test flow reconstruction for a large-scale expansion tube, part 1: quasi-one-dimensional modelling

2017

Journal Article

Application of a wall function to simulate turbulent flows in foil bearings at high rotational speeds

Qin, Kan, Gollan, Rowan J. and Jahn, Ingo H. (2017). Application of a wall function to simulate turbulent flows in foil bearings at high rotational speeds. Tribology International, 115, 546-556. doi: 10.1016/j.triboint.2017.06.018

Application of a wall function to simulate turbulent flows in foil bearings at high rotational speeds

2017

Journal Article

Numerical study of the effect of wall temperature profiles on the premixed methane–air flame dynamics in a narrow channel

Kang, Xin, Gollan, Rowan J., Jacobs, Peter A. and Veeraragavan, Ananthanarayanan (2017). Numerical study of the effect of wall temperature profiles on the premixed methane–air flame dynamics in a narrow channel. RSC Advances, 7 (63), 39940-39954. doi: 10.1039/C7RA07265A

Numerical study of the effect of wall temperature profiles on the premixed methane–air flame dynamics in a narrow channel

2017

Journal Article

On the influence of modelling choices on combustion in narrow channels

Kang, Xin, Gollan, Rowan J., Jacobs, Peter A. and Veeraragavan, Ananthanarayanan (2017). On the influence of modelling choices on combustion in narrow channels. Computers and Fluids, 144, 117-136. doi: 10.1016/j.compfluid.2016.11.017

On the influence of modelling choices on combustion in narrow channels

2017

Journal Article

Effect of vortex-injection interaction on wall heat transfer in a flat plate with fin corner geometry

Llobet, Juan R., Gollan, Rowan J. and Jahn, Ingo H. (2017). Effect of vortex-injection interaction on wall heat transfer in a flat plate with fin corner geometry. Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 15 (No.APISAT-2016), a17-a26. doi: 10.2322/tastj.15.a17

Effect of vortex-injection interaction on wall heat transfer in a flat plate with fin corner geometry

2017

Conference Publication

Numerical modeling and simulation of supersonic flows in propulsion systems by open-source solvers

Hoste, Jimmy-John O.E., Casseau, Victor, Fossati, Marco, Taylor, Ian J. and Gollan, Rowan J. (2017). Numerical modeling and simulation of supersonic flows in propulsion systems by open-source solvers. 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-2411

Numerical modeling and simulation of supersonic flows in propulsion systems by open-source solvers

2017

Conference Publication

Effect of Vortex-injection Interaction on Wall Heat Transfer in a Flat Plate and Fin Corner Geometry

Llobet, Juan R., Gollan, Rowan J. and Jahn, Ingo H. (2017). Effect of Vortex-injection Interaction on Wall Heat Transfer in a Flat Plate and Fin Corner Geometry. Asia-Pacific International Symposium on Aerospace Technology, Toyama, Japan, 25-27 October 2016. Toyama, Japan: Japan Society for Aeronautical and Space Sciences (JSASS).

Effect of Vortex-injection Interaction on Wall Heat Transfer in a Flat Plate and Fin Corner Geometry

2017

Conference Publication

Preliminary experimental investigation of air radiation in super-orbital expanding flow

Wei, H., Morgan, R. G., Sheikh, U. A., Jacobs, P. A., Gollan, R. J. and McIntyre, T. J. (2017). Preliminary experimental investigation of air radiation in super-orbital expanding flow. International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-44866-4_8

Preliminary experimental investigation of air radiation in super-orbital expanding flow

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

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Supervision history

Current supervision

  • Doctor Philosophy

    Tailoring surface conditions to control transition in hypersonic boundary layers

    Principal Advisor

    Other advisors: Dr Nick Gibbons

  • Doctor Philosophy

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

    Principal Advisor

  • Doctor Philosophy

    Shape Morphing Hypersonic Vehicles

    Principal Advisor

    Other advisors: Professor Vincent Wheatley

  • Doctor Philosophy

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

    Principal Advisor

  • 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

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

    Principal Advisor

    Other advisors: Dr Chris James, Dr Nick Gibbons

  • 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

    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

    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

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

    Associate Advisor

    Other advisors: Professor Vincent Wheatley

  • 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

  • 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

Media

Enquiries

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