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Dr Rowan Gollan
Dr

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

Dr 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

101 works between 2001 and 2024

1 - 20 of 101 works

2024

Conference Publication

Numerical study of magnetic field deformation for a blunt body with an applied magnetic field during atmospheric entry

van Oeveren, Sebastiaan B., Gildfind, David, Wheatley, Vincent, Gollan, Rowan and Jacobs, Peter (2024). Numerical study of magnetic field deformation for a blunt body with an applied magnetic field during atmospheric entry. AIAA SCITECH 2024 Forum, Orlando, FL, United States, 8-12 January 2024. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2024-1646

Numerical study of magnetic field deformation for a blunt body with an applied magnetic field during atmospheric entry

2024

Conference Publication

Adjoint differentiation method for trajectory simulations with terminal conditions

Mittelman, Amir, Jahn, Ingo and Gollan, Rowan (2024). Adjoint differentiation method for trajectory simulations with terminal conditions. 63rd Israel Annual Conference on Aerospace Sciences 2024, Haifa, Israel, 9 May 2024. Haifa, Israel: Technion Israel Institute of Technology.

Adjoint differentiation method for trajectory simulations with terminal conditions

2024

Conference Publication

Modular Modelling Approach for Efficient Gradient Evaluation of a Low-Order Integrated Scramjet Propulsion System

Mittelman, Amir, Mackle, Kieran, Jahn, Ingo and Gollan, Rowan (2024). Modular Modelling Approach for Efficient Gradient Evaluation of a Low-Order Integrated Scramjet Propulsion System. Technion Israel Institute of Technology.

Modular Modelling Approach for Efficient Gradient Evaluation of a Low-Order Integrated Scramjet Propulsion System

2023

Conference Publication

Effect of magnetohydrodynamic aerobraking on flow field surrounding an Earth re-entry capsule

Gildfind, D., Jacobs, P., Lefevre, A. and Gollan, R. (2023). Effect of magnetohydrodynamic aerobraking on flow field surrounding an Earth re-entry capsule. 34th International Symposium on Shock Waves (ISSW34), Daegu, Korea, 16-21 July 2023.

Effect of magnetohydrodynamic aerobraking on flow field surrounding an Earth re-entry capsule

2023

Journal Article

Correction: Magnetohydrodynamic Experiments of Total Heat Flux Mitigation for Superorbital Earth Reentry

Lefevre, Alexis, Gildfind, David E., Gollan, Rowan J., Jacobs, Peter A. and James, Christopher M. (2023). Correction: Magnetohydrodynamic Experiments of Total Heat Flux Mitigation for Superorbital Earth Reentry. AIAA Journal, 61 (6), 1-1. doi: 10.2514/1.j061771.c1

Correction: Magnetohydrodynamic Experiments of Total Heat Flux Mitigation for Superorbital Earth Reentry

2023

Journal Article

Correction: Expansion Tube Experiments of Magnetohydrodynamic Aerobraking for Superorbital Reentry

Lefevre, Alexis, Gildfind, David E., Gollan, Rowan J., Jacobs, Peter A., McIntyre, Timothy J. and James, Christopher M. (2023). Correction: Expansion Tube Experiments of Magnetohydrodynamic Aerobraking for Superorbital Reentry. AIAA Journal, 61 (4), 1-1. doi: 10.2514/1.j060253.c1

Correction: Expansion Tube Experiments of Magnetohydrodynamic Aerobraking for Superorbital Reentry

2023

Conference Publication

Correction: Aerodynamic Effects and Heat Flux Augmentation of a Transpiration Cooled Hypersonic Sharp Leading Edge

Ravichandran, Raghul, Doherty, Luke J., McGilvray, Matthew, Damm, Kyle and Gollan, Rowan (2023). Correction: Aerodynamic Effects and Heat Flux Augmentation of a Transpiration Cooled Hypersonic Sharp Leading Edge. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0437.c1

Correction: Aerodynamic Effects and Heat Flux Augmentation of a Transpiration Cooled Hypersonic Sharp Leading Edge

2023

Conference Publication

Application of a Jacobian-free Newton-Krylov method to the simulation of hypersonic flows

Damm, Kyle A., Gibbons, Nicholas N., Jacobs, Peter A. and Gollan, Rowan (2023). Application of a Jacobian-free Newton-Krylov method to the simulation of hypersonic flows. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-2295

Application of a Jacobian-free Newton-Krylov method to the simulation of hypersonic flows

2023

Conference Publication

Walsh functions for shock tracking and their application to expansion tube simulations

Border, Jamie and Gollan, Rowan (2023). Walsh functions for shock tracking and their application to expansion tube simulations. AIAA SCITECH 2023 Forum, National Harbor, MD, United States, 23-27 January 2023. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-2631

Walsh functions for shock tracking and their application to expansion tube simulations

2023

Conference Publication

Aerodynamic Effects of Blowing on a Sharp, Slender Hypersonic Leading Edge

Ravichandran, Raghul, Doherty, Luke J., McGilvray, Matthew, Damm, Kyle and Gollan, Rowan (2023). Aerodynamic Effects of Blowing on a Sharp, Slender Hypersonic Leading Edge. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0437

Aerodynamic Effects of Blowing on a Sharp, Slender Hypersonic Leading Edge

2023

Conference Publication

Trajectory-Based Conjugate Heat Transfer Simulation of the BoLT-II Flight Experiment

Damm, Kyle A., Gollan, Rowan and Veeraragavan, Anand (2023). Trajectory-Based Conjugate Heat Transfer Simulation of the BoLT-II Flight Experiment. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0292

Trajectory-Based Conjugate Heat Transfer Simulation of the BoLT-II Flight Experiment

2023

Conference Publication

Feasibility of MHD aerobraking for use in Martian atmospheric entry

Ogilvie, John C., Gildfind, David, Gollan, Rowan and Gibbons, Nicholas N. (2023). Feasibility of MHD aerobraking for use in Martian atmospheric entry. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-2560

Feasibility of MHD aerobraking for use in Martian atmospheric entry

2023

Conference Publication

Simulation of multiple instabilities in the entropy layer over a hypersonic blunt cone

Whyborn, Lachlan S., Gollan, Rowan and Jacobs, Peter A. (2023). Simulation of multiple instabilities in the entropy layer over a hypersonic blunt cone. AIAA SCITECH 2023 Forum, National Harbor, MD, United States and online, 23-27 January 2023. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0474

Simulation of multiple instabilities in the entropy layer over a hypersonic blunt cone

2023

Journal Article

Eilmer: an open-source multi-physics hypersonic flow solver

Gibbons, Nicholas N., Damm, Kyle A., Jacobs, Peter A. and Gollan, Rowan J. (2023). Eilmer: an open-source multi-physics hypersonic flow solver. Computer Physics Communications, 282 108551, 1-20. doi: 10.1016/j.cpc.2022.108551

Eilmer: an open-source multi-physics hypersonic flow solver

2022

Journal Article

Computational analysis of experiments on shock detachment in hypersonic flow of nitrogen and carbon dioxide over a wedge

Hornung, H.G., Gollan, R.J. and Jacobs, P.A. (2022). Computational analysis of experiments on shock detachment in hypersonic flow of nitrogen and carbon dioxide over a wedge. Journal of Fluid Mechanics, 951 A6. doi: 10.1017/jfm.2022.838

Computational analysis of experiments on shock detachment in hypersonic flow of nitrogen and carbon dioxide over a wedge

2022

Journal Article

Magnetohydrodynamic experiments of total heat flux mitigation for superorbital earth reentry

Lefevre, Alexis, Gildfind, David E., Gollan, Rowan J., Jacobs, Peter A. and James, Christopher M. (2022). Magnetohydrodynamic experiments of total heat flux mitigation for superorbital earth reentry. AIAA Journal, 60 (9), 1-14. doi: 10.2514/1.j061771

Magnetohydrodynamic experiments of total heat flux mitigation for superorbital earth reentry

2022

Journal Article

Correlation for species concentration on a hypersonic stagnation point with mass injection

Rocher, Marc Ewenz, Hermann, Tobias, McGilvray, Matthew and Gollan, Rowan (2022). Correlation for species concentration on a hypersonic stagnation point with mass injection. AIAA Journal, 60 (5), 2798-2809. doi: 10.2514/1.J061159

Correlation for species concentration on a hypersonic stagnation point with mass injection

2022

Journal Article

Electron number density measurements in a Saturn entry condition

Liu, Yu, James, Christopher M., Morgan, Richard G., Jacobs, Peter A., Gollan, Rowan and McIntyre, Timothy J. (2022). Electron number density measurements in a Saturn entry condition. AIAA Journal, 60 (3), 1303-1315. doi: 10.2514/1.j060560

Electron number density measurements in a Saturn entry condition

2022

Journal Article

A design method for three-dimensional scramjet nozzles with shape transition

Kunze, Jens, Smart, Michael K. and Gollan, Rowan (2022). A design method for three-dimensional scramjet nozzles with shape transition. Journal of Propulsion and Power, 38 (1), 3-17. doi: 10.2514/1.b38293

A design method for three-dimensional scramjet nozzles with shape transition

2022

Conference Publication

Experimental measurements of total heat flux for superorbital earth reentry with magnetohydrodynamic flow control

Lefevre, Alexis, Gildfind, David E., Gollan, Rowan J., Jacobs, Peter A., James, Christopher M. and McIntyre, Timothy J. (2022). Experimental measurements of total heat flux for superorbital earth reentry with magnetohydrodynamic flow control. AIAA SCITECH Forum, San Diego, CA, United States & Virtual, 3-7 January 2022. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2022-0828

Experimental measurements of total heat flux for superorbital earth reentry with magnetohydrodynamic flow control

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
  • 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

Supervision

Availability

Dr Rowan Gollan is:
Available for supervision

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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

    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

    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

Media

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