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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

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

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

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

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

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

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

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

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