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2015 Conference Publication Shock standoff on hemi-spherical bodies in hypervelocity flowsZander, F., Jacobs, P. A., Gollan, R. J. and Morgan, R. G. (2015). Shock standoff on hemi-spherical bodies in hypervelocity flows. International Symposium on Shock Waves (ISSW29), Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_85 |
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2014 Conference Publication Numerical simulations of premixed combustion in narrow channelsKang, 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. |
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2013 Conference Publication Design, operation and testing in expansion tube facilities for super-orbital re-entryJacobs, 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. |
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2012 Conference Publication On the validation of a hypersonic flow solver using measurements of shock detachment distanceGollan, 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. |
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2012 Conference Publication High temperature gas effects for converging conical shocksZander, 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 |
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2012 Conference Publication Verification of a compressible flow solverGollan, 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. |
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2012 Conference Publication Mach disk platform for studying radiating flowsZander, 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 . |
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2011 Conference Publication Investigation of REST-class hypersonic inlet designsGollan, 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 |
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2010 Conference Publication Adaption and use of a compressible flow code for turbomachinery designVentura, 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. |
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2010 Conference Publication CFD Tools for Design and Simulation of Transient Flows in Hypersonic FacilitiesJacobs, 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. |
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2010 Conference Publication Design of modular shape-transitioning inlets for a conical hypersonic vehicleGollan, 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 |
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2009 Conference Publication A simulation technique for radiating shock tube flowsRowan 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 |
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2009 Conference Publication Numerical simulations and analysis of the 8.5 km/s CO2-N2 east shock tube conditionPotter, 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. |
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2008 Conference Publication Impulse facilities for the simulation of hypersonic radiating flowsMorgan, 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 |
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2008 Conference Publication Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layersPotter, 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. |
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2007 Conference Publication Development of Casbar: a Two-phase Flow Code for the Interior Ballistics ProblemGollan, 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. |
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2007 Conference Publication Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layersPotter, 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. |
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2006 Conference Publication Impulse facility simulation of hypervelocity radiating flowsBrandis, 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. |
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2006 Conference Publication Expansion tube operating conditions for studying nonequilibrium radiation relevant to Titan AerocaptureBrandis, 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. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, California, USA, 9-12 July 2006. USA: American Institute of Aeronautics and Astronautics. |
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2006 Conference Publication Analytical maps of aerodynamic damping as a function of operating condition for a compressor profilePetrie-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 |
