Skip to menu Skip to content Skip to footer

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

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

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

2007

Conference Publication

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. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 2-7 December 2007. Brisbane, Australia: School of Engineering, The University of Queensland.

Development of Casbar: a Two-phase Flow Code for the Interior Ballistics Problem

2007

Conference Publication

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. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Queensland: School of Engineering, The University of Queensland.

Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers

2006

Conference Publication

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. 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Rome, Italy, 6-8 September 2006. The Netherlands: ESA Publications.

Impulse facility simulation of hypervelocity radiating flows

2006

Conference Publication

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. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, CA, United States, 5-8 June 8 2006. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2006-2958

Radiation measurements in nonreflected shock tunnels

2006

Conference Publication

Expansion tube operating conditions for studying nonequilibrium radiation relevant to Titan Aerocapture

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. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, California, USA, 9-12 July 2006. USA: American Institute of Aeronautics and Astronautics.

Expansion tube operating conditions for studying nonequilibrium radiation relevant to Titan Aerocapture

2006

Conference Publication

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. TE06: ASME Turbo Expo 2006, Barcelona, Spain, 8-11 May 2006. New York, NY, U.S.A.: ASME. doi: 10.1115/GT2006-90829

Analytical maps of aerodynamic damping as a function of operating condition for a compressor profile

2006

Conference Publication

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. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, California, USA, 5-8 June 2006. Reston, VA, U.S.A.: American Institute of Aeronautics and Astronautics.

Radiation measurements in nonreflected shock tunnels

2005

Conference Publication

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. 43rd AIAA Aerospace Science Meeting and Exhibit, Reno, Nevada, United States, 10 - 13 January 2005. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2005-694

Superorbital expansion tube operation: estimates of flow conditions via numerical simulation

2004

Journal Article

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.

Numerical modelling of radiating superorbital flows

2003

Other Outputs

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..

Yet another finite-rate chemistry module for compressible flow codes

2003

Other Outputs

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..

Numerical modelling of radiating superorbital flows: with detailed governing equations