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.
Journal Article: Effect of scramjet inlet vortices on fuel plume elongation and mixing rate
Llobet, J. R., Gollan, R. J. and Jahn, I. H. (2019) Effect of scramjet inlet vortices on fuel plume elongation and mixing rate. The Aeronautical Journal, 1-21. doi:10.1017/aer.2019.45
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
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. In: Akihiro Sasoh, Toshiyuki Aoki and Masahide Katayama, 31st International Symposium on Shock Waves 2: Applications. 31st International Symposium on Shock Waves, Nagoya, Japan, (197-204). 9-14 July 2017. doi:10.1007/978-3-319-91017-8_24
Non-equilibrium reacting shock layers
(2020–2022) ARC Discovery Projects
Electron Transpiration Cooling of Hypersonic Vehicles
(2019–2022) ARC Linkage Projects
Study of Non-Equilibrium Wakes Model
(2019–2021) Asian Office of Aerospace Research and Development
ADJOINT-BASED AERODYNAMIC DESIGN OPTIMISATION IN HYPERSONIC FLOW
Doctor Philosophy
Radiating flows
Doctor Philosophy
Walsh functions for high-resolution shock capturing and their application to expansion tube simulations
Doctor Philosophy
Effect of scramjet inlet vortices on fuel plume elongation and mixing rate
Llobet, J. R., Gollan, R. J. and Jahn, I. H. (2019) Effect of scramjet inlet vortices on fuel plume elongation and mixing rate. The Aeronautical Journal, 1-21. doi:10.1017/aer.2019.45
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
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
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
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
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
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
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
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
Kang, X., Gollan, R., Jacobs, P. A. and Veeraragavan, A. (2016) Suppression of instabilities in a premixed methane–air flame in a narrow channel via hydrogen/carbon monoxide addition. Combustion and Flame, 173 266-275. doi:10.1016/j.combustflame.2016.07.003
Development of a computational tool to simulate foil bearings for supercritical CO2 cycles
Qin, Kan, Jahn, Ingo, Gollan, Rowan and Jacobs, Peter (2016) Development of a computational tool to simulate foil bearings for supercritical CO2 cycles. Journal of Engineering for Gas Turbines and Power, 138 9: 092503-1-092503-19. doi:10.1115/1.4032740
Use of the method of manufactured solutions for the verification of conjugate heat transfer solvers
Veeraragavan, A., Beri, J. and Gollan, R. J. (2016) Use of the method of manufactured solutions for the verification of conjugate heat transfer solvers. Journal of Computational Physics, 307 308-320. doi:10.1016/j.jcp.2015.12.004
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
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
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
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.
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
Numerical modelling of radiating superorbital flows
Gollan, R. J., Jacobs, P. A., Karl, S. and Smith, S. C. (2004) Numerical modelling of radiating superorbital flows. ANZIAM Journal, 45 E: C248-C268.
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. In: Akihiro Sasoh, Toshiyuki Aoki and Masahide Katayama, 31st International Symposium on Shock Waves 2: Applications. 31st International Symposium on Shock Waves, Nagoya, Japan, (197-204). 9-14 July 2017. doi:10.1007/978-3-319-91017-8_24
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. In: AIAA Scitech 2019 Forum, San Diego, CA, United States, (). 7-11 January 2019. doi:10.2514/6.2019-0796
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. In: 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018, Orlando, FL, United States, (). September 17, 2018-September 19, 2018. doi:10.2514/6.2018-5318
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. In: 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018, Orlando, FL, United States, (). September 17, 2018-September 19, 2018. doi:10.2514/6.2018-5270
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. In: 21st Australasian Fluid Mechanics Conference, Adelaide, SA, Australia, (). 10-13 December 2018.
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. In: Proceedings of the 8th Asia-Pacific International Symposium on Aerospace Technology (APISAT). Asia-Pacific International Symposium on Aerospace Technology, Toyama, Japan, (). 25-27 October 2016.
Modeling scramjet supersonic combustion via eddy dissipation model
Hoste, Jimmy-John O.E., Fossati, Marco, Taylor, Ian J. and Gollan, Rowan J. (2017). Modeling scramjet supersonic combustion via eddy dissipation model. In: 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017, Adelaide, SA, Australia, (9165-9177). 25-29 September 2017.
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. In: 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017. 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, (). 6-9 March 2017. doi:10.2514/6.2017-2411
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. In: Gabi Ben-Dor, Ozer Igra and Oren Sadot, 30th International Symposium on Shock Waves 2: ISSW30-Volume 1. International Symposium on Shock Waves, Tel Aviv, Israel, (827-831). 19-24 July 2015. doi:10.1007/978-3-319-44866-4_8
Experimental and computational fluid dynamics studies of superorbital earth re-entry
Fahy, Elise J., Gollan, Rowan J., Buttsworth, David R., Jacobs, Peter A. and Morgan, Richard G. (2016). Experimental and computational fluid dynamics studies of superorbital earth re-entry. In: 46th AIAA Thermophysics Conference. 46th AIAA Thermophysics Conference, Washington, DC, United States, (). 13 - 17 June 2016. doi:10.2514/6.2016-3532
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. In: 20th Australasian Fluid Mechanics Conference. 20th Australasian Fluid Mechanics Conference, Perth, Australia, (). 5 – 8 December 2016.
On the effect of workload ordering for reacting flow simulations using GPUs
Damm, K. A., Gollan, R. J. and Veeraragavan, A. (2016). On the effect of workload ordering for reacting flow simulations using GPUs. In: 20th Australasian Fluid Mechanics Conference. 20th Australasian Fluid Mechanics Conference, Perth, Australia, (). 5 – 8 December 2016.
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. In: 20th Australasian Fluid Mechanics Conference. 20th Australasian Fluid Mechanics Conference, Perth, Australia, (). 5 – 8 December 2016.
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. In: Proceedings of the 20th Australasian Fluid Mechanics Conference, AFMC 2016. 20th Australasian Fluid Mechanics Conference, Perth, Australia, (). 5-8 December 2016.
Acceleration of combustion simulations using GPUs
Damm, K. A., Gollan, R. J. and Veeraragavan, A. (2015). Acceleration of combustion simulations using GPUs. In: Yi Yang and Nigel Smith, The Australian Combustion Symposium 2015 Proceedings. Australian Combustion Symposium, Parkville, VIC, Australia, (148-151). 7-9 December 2015.
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. In: International Space Planes and Hypersonic Systems and Technologies Conferences. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, (). 6-9 July 2015. doi:10.2514/6.2015-3597
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. In: ACCM2015 2nd Australasian Conference on Computational Mechanics. Australasian Conference on Computational Mechanics, Brisbane, Australia, (). 30 November to 1 December 2015.
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. In: Yi Yang and Nigel Smith, The Australian Combustion Symposium 2015 Proceedings. Australian Combustion Symposium, Parkville, VIC, Australia, (388-391). 7-9 December 2015.
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. In: Riccardo Bonazza and Devesh Ranjan, 29th International Symposium on Shock Waves 1. International Symposium on Shock Waves (ISSW29), Madison, WI, United States, (539-544). 14-19 July 2013. doi:10.1007/978-3-319-16835-7_85
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. In: Harun Chowdhury and Firoz Alam, The Proceedings of the 19th Australasian Fluid Mechanics Conference. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, (). 8-11 December 2014.
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. In: O. Chazot and T. Magin, STO-AVT-VKI Lecture Series Radiation and Gas-Surface Interaction Phenomena in High Speed Re-Entry (2013-AVT-218), Rhode-St-Genèse, Belgium, (5-1-5-65). 6-8 May 2013.
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. In: 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, (). 24 - 28 September 2012. doi:10.2514/6.2012-5939
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. In: L. Ouwehand, Proceedings of 5th International Workshop Radiation of High Temperature Gases in Atmospheric Entry. 5th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Barcelona, Spain, (). 16-19 October 2012.
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. In: Konstantinos Kontis, 28th International Symposium on Shock Waves Vol 1 and 2. International Symposium on Shock Waves (28th, ISSW28), Manchester, U.K., (). 17-22 July 2011.
Verification of a compressible flow solver
Gollan, R. J. and Jacobs, P. A. (2012). Verification of a compressible flow solver. In: P. A. Brandner, B. W. Pearce and Hawthorn, VIC, Australia, Proceedings of the 18th Australasian Fluid Mechanics Conference. 18th Australasian Fluid Mechanics Conference (AFMC), Launceston, Australia, (). 3-7 December 2012.
Investigation of REST-class hypersonic inlet designs
Gollan, Rowan J. and Ferlemann, Paul G. (2011). Investigation of REST-class hypersonic inlet designs. In: 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011, , , (). April 11, 2011-April 14, 2011. doi:10.2514/6.2011-2254
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. In: J. C. F. Pereira and A. Sequeira, V European Conference on Computational Fluid Dynamics ECCOMAS CFD, Lisbon, Portugal, (). 14-17 June 2010.
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. In: VKI RTO Proceedings. AVT-186 RTO AVT/VKI Lecture Series - Aerothermodynamic design, review on ground testing and CFD, Genese, Belgium, (). 29 March-01 April 2010.
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. In: Proceedings of the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, United States, (1-15). 4-7 January 2010.
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. In: Dr Klaus Hannemann and Prof Friedrich Seile, Shock Waves. 26th International Symposium on Shock Waves (ISSW26), Gottingen, Germany, (465-470). 15-20 July. doi:10.1007/978-3-540-85168-4_74
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. In: Huguette Sawaya-Lacoste and L. Ouwehand, Proceedings of the 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry. 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Heraklion, Greece, (). 30 September - 3 October 2008.
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. In: Proceedings of: 38th Fluid Dynamics Conference and Exhibit. 38th Fluid Dynamics Conference and Exhibit, Seattle, Washington, U.S.A., (1-16). 23 - 26 June, 2008.
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. In: Advancing the Science of Flight Technology.. 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, (1280-1296). 7-10 january 2008.
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. In: Peter Jacobs, Tim McIntyre, Matthew Cleary, David Buttsworth, David Mee, Rose Clements, Richard Morgan and Charles Lemckert, 16th Australasian Fluid Mechanics Conference (AFMC). 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, (295-302). 2-7 December 2007.
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. In: Peter Jacobs, Tim McIntyre, Matthew Cleary, David Buttsworth, David Mee, Rose Clements, Richard Morgan and Charles Lemckert, 16th Australasian Fluid Mechanics Conference (AFMC). 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, (373-380). 3-7 December, 2007.
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. In: Proceedings of the GT2006 ASME Turbo Expo 2006: Power for Land, Sea and Air.. TE06: ASME Turbo Expo 2006, Barcelona, Spain, (1133-1144). 8-11 May 2006. doi:10.1115/GT2006-90829
Brandis, A. M., Gollan, R. J., Scott, M. P., Morgan, R. G. and Jacobs, P. A. (2006). Expansion tube operating conditions for studying nonequilibrium radiation relevant to Titan Aerocapture. In: Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, California, USA, (2074-2083). 9-12 July 2006.
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. In: Proceedings of the 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry. 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Rome, Italy, (1-6). 6-8 September 2006.
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. In: 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, California, USA, (1-9). 5-8 June 2006.
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 V. and Wright, Michael (2006). Radiation measurements in nonreflected shock tunnels. In: Collection of Technical Papers - 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, CA, United States, (224-232). 5-8 June 8 2006. doi:10.2514/6.2006-2958
Superorbital expansion tube operation: estimates of flow conditions via numerical simulation
Jacobs, P. A., Silvester, T. B., Morgan, R. G., Scott ,M .P., Gollan, R. J. and McIntyre, T. J. (2005). Superorbital expansion tube operation: estimates of flow conditions via numerical simulation. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers. 43rd AIAA Aerospace Science Meeting and Exhibit, Reno, Nevada, United States, (13627-13635). 10 - 13 January 2005.
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 St Lucia, QLD, Australia:
Computational Modelling of High-Temperature Gas Effects with Application to Hypersonic Flows
Rowan Gollan (2008). Computational Modelling of High-Temperature Gas Effects with Application to Hypersonic Flows PhD Thesis, School of Engineering, The University of Queensland.
Numerical modelling of radiating superorbital flows: with detailed governing equations
Gollan, R. J. and Jacobs, P.A. (2003) Numerical modelling of radiating superorbital flows: with detailed governing equations St. Lucia: Div. of Mech. Eng., The Univ. of Qld.
Yet another finite-rate chemistry module for compressible flow codes
Gollan, R. J. (2003) Yet another finite-rate chemistry module for compressible flow codes St. Lucia: Div. of Mech. Eng., The Univ. of Qld.
Implementation of subsonic boundary conditions in compressible flow codes
Gollan, Rowan (2001). Implementation of subsonic boundary conditions in compressible flow codes B.Sc Thesis, School of Engineering, The University of Queensland.
Non-equilibrium reacting shock layers
(2020–2022) ARC Discovery Projects
Electron Transpiration Cooling of Hypersonic Vehicles
(2019–2022) ARC Linkage Projects
Study of Non-Equilibrium Wakes Model
(2019–2021) Asian Office of Aerospace Research and Development
Functional Representation of Generic Surfaces for CFD Applications
(2018) Commonwealth Defence Science and Technology Group
CRC - Project: Advanced manufacturing approaches for high power dense motors
(2017–2019) Cooperative Research Centre Projects
Experimental Studies of High-Speed Flows
(2017–2019) National University of Singapore Research Collaboration Agreement
Turbulent heat transfer during Mars Venus and Earth atmospheric entry
(2017–2019) ARC Discovery Projects
Rapidly expanding non equilibrium hypersonic flow
(2016–2019) Asian Office of Aerospace Research and Development
Development of computer-based optimisation to improve hypersonic aerodynamic design.
(2014–2017) ARC Discovery Early Career Researcher Award
A parallel computer facility for modelling and simulation
(2014) UQ Major Equipment and Infrastructure
(2006–2007) Department Defence - Defence Science & Technology
ADJOINT-BASED AERODYNAMIC DESIGN OPTIMISATION IN HYPERSONIC FLOW
Doctor Philosophy — Principal Advisor
Other advisors:
Radiating flows
Doctor Philosophy — Principal Advisor
Other advisors:
Walsh functions for high-resolution shock capturing and their application to expansion tube simulations
Doctor Philosophy — Principal Advisor
Other advisors:
Co-design of control and vehicle geometry for hypersonics
Doctor Philosophy — Associate Advisor
Other advisors:
Infrared Thermography in Expansion Tunnels
Doctor Philosophy — Associate Advisor
Other advisors:
Two-fluid modeling of electron transpiration cooling for the leading edges of hypersonic vehicles
Doctor Philosophy — Associate Advisor
Other advisors:
Direct Numerical Simulation of Transition to Turbulence on Aeroshells
Doctor Philosophy — Associate Advisor
Other advisors:
Multi-disciplinary design of an accelerating hypersonic vehicle
Doctor Philosophy — Associate Advisor
Other advisors:
Design of a variable Mach number scramjet flowpath for access to space.
Doctor Philosophy — Associate Advisor
Other advisors:
(2019) Doctor Philosophy — Associate Advisor
Other advisors:
(2018) Doctor Philosophy — Associate Advisor
Other advisors:
Micro/mesoscale Combustion Based Portable Power Generating System
(2017) Doctor Philosophy — Associate Advisor
Other advisors:
Numerical Study into Thermal-Compression Scramjets
(2015) Doctor Philosophy — Associate Advisor