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2010

Conference Publication

Modeling of radiating flows in the atmospheres of the Gas Giants

Morgan, R. G. (2010). Modeling of radiating flows in the atmospheres of the Gas Giants. 17th Australasian Fluid Mechanics Conference 2010, 17AFMC, Auckland, New Zealand, 5 - 9 December 2010. Auckland NZ: University of Auckland, Dept. of Mechanical Engineering.

Modeling of radiating flows in the atmospheres of the Gas Giants

2010

Conference Publication

Design of lightweight pistons for the X2 and X3 expansion tube free-piston drivers

Gildfind, D. E., Morgan, R. G., McGilvray, M., Jacobs, P. A., Eichmann, T., Stalker, R. J. and Teakle, P. (2010). Design of lightweight pistons for the X2 and X3 expansion tube free-piston drivers. 17AFMC: 17th Australasian Fluid Mechanics Conference, Auckland, New Zealand, 5-9 December 2010. Auckland, New Zealand: The University of Auckland.

Design of lightweight pistons for the X2 and X3 expansion tube free-piston drivers

2010

Conference Publication

Expansion tunnel radiation experiments to support hayabusa re-entry observations

Buttsworth, David R., D'Souza, Mary, Potter, Daniel, Eichmann, Troy N., Mudford, Neil, McGilvray, Matthew, McIntyre, Timothy J., Jacobs, Peter A. and Morgan, Richard G. (2010). Expansion tunnel radiation experiments to support hayabusa re-entry observations. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, USA, 4-7 January 2010. Reston, VA, United States: American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/6.2010-634

Expansion tunnel radiation experiments to support hayabusa re-entry observations

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

Journal Article

Diagnostic modelling of an expansion tube operating condition

McGilvray, M., Austin, J. M., Sharma, M., Jacobs, P. A. and Morgan, R. G. (2009). Diagnostic modelling of an expansion tube operating condition. Shock Waves, 19 (1), 59-66. doi: 10.1007/s00193-009-0187-9

Diagnostic modelling of an expansion tube operating condition

2009

Journal Article

Effects of Upstream Injection on Scramjet Performance Using an Entropy-Based Method

McGilvray, M and Morgan, RG (2009). Effects of Upstream Injection on Scramjet Performance Using an Entropy-Based Method. JOURNAL OF PROPULSION AND POWER, 25 (2), 295-302. doi: 10.2514/1.38325

Effects of Upstream Injection on Scramjet Performance Using an Entropy-Based Method

2009

Conference Publication

Overview of radiation intensity measurements on the x2 facility at the university of queensland

Brandis, A., McIntyre, T., Morgan, R. and Jacobs, P. (2009). Overview of radiation intensity measurements on the x2 facility at the university of queensland. 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Heraklion, Greece, 30 September – 3 October 2008. Noordwijk, The Netherlands: European Space Agency.

Overview of radiation intensity measurements on the x2 facility at the university of queensland

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

Radiatively cooled scramjet combustor

Morgan, R. G. and Zander, F. (2009). Radiatively cooled scramjet combustor. 26th International Symposium on Shock Waves (ISSW26), Gottingen, Germany, 15-20 July 2007. Berlin, Germany: Springer. doi: 10.1007/978-3-540-85181-3_55

Radiatively cooled scramjet combustor

2009

Conference Publication

The generation and measurement of high temperature radiating flows in a high enthalpy pulsed facility

McIntyre, T. J., Eichmann, T. N., Mallon, M., Potter, D., Brandis, A., Jacobs, C., Morgan, R., Jacobs, P. and Buttsworth, D. (2009). The generation and measurement of high temperature radiating flows in a high enthalpy pulsed facility. 3rd International Workshop: Radiation of High Temperature Gases in Atmospheric Entry, Heraklion, Greece, 30 September - 3 October 2008. Noordwijk, The Netherlands: ESA Communication Production Office.

The generation and measurement of high temperature radiating flows in a high enthalpy pulsed facility

2009

Conference Publication

Composite scramjet combustor

Zander, Fabian and Morgan, Richard (2009). Composite scramjet combustor. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, 19 - 22 October 2009. Reston, VA United States: AIAA. doi: 10.2514/6.2009-7354

Composite scramjet combustor

2009

Conference Publication

Scramjet experiments in an expansion tunnel: Evaluated using a quasi- steady analysis technique

McGilvray, Matthew, Morgan, Richard G. and Jacobs, Peter A. (2009). Scramjet experiments in an expansion tunnel: Evaluated using a quasi- steady analysis technique. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, 19-22 October, 2009. Washington, DC, U.S.A.: AIAA - American Institute of Aeronautics and Astronautics. doi: 10.2514/1.J050024

Scramjet experiments in an expansion tunnel: Evaluated using a quasi- steady analysis technique

2009

Conference Publication

Nonequilibrium radiation modeling and experimentation relevant to titan entry

Brandis, Aaron, McIntyre, Tim, Morgan, Richard, Jacobs, Peter, Laux, Christophe and Magin, Thierry (2009). Nonequilibrium radiation modeling and experimentation relevant to titan entry. 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry , Heraklion, Greece, 30 September-3 October 2008. Noordwijik, The Netherlands: ESA Communication Production Office.

Nonequilibrium radiation modeling and experimentation relevant to titan entry

2009

Conference Publication

Radiation measurements in rarefied Titan atmospheres

Jacobs, C. M. and Morgan, R. G. (2009). Radiation measurements in rarefied Titan atmospheres. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, FL, 5 - 8 January 2009. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2009-1029

Radiation measurements in rarefied Titan atmospheres

2009

Conference Publication

Experimental investigation of the effect of two incident shock waves on a turbulent boundary layer in hypersonic circular duct flows

Dann, A. G. and Morgan, R. G. (2009). Experimental investigation of the effect of two incident shock waves on a turbulent boundary layer in hypersonic circular duct flows. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition [Papers], Orlando, FL United States, 5 - 8 January 2009. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2009-33

Experimental investigation of the effect of two incident shock waves on a turbulent boundary layer in hypersonic circular duct flows

2008

Journal Article

Skin-friction measurements and flow establishment within a long duct at superorbital speeds

Silvester, T. B. and Morgan, R. G. (2008). Skin-friction measurements and flow establishment within a long duct at superorbital speeds. AIAA Journal, 46 (2), 527-536. doi: 10.2514/1.32668

Skin-friction measurements and flow establishment within a long duct at superorbital speeds

2008

Conference Publication

Skin-friction measurements and flow establishment within a long duct at superorbital speeds

Silvester, T. B. and Morgan, R. G. (2008). Skin-friction measurements and flow establishment within a long duct at superorbital speeds. doi: 10.2514/1.32668

Skin-friction measurements and flow establishment within a long duct at superorbital speeds

2008

Conference Publication

Nonequilibrium radiation intensity measurements in simulated Titan atmospheres

Brandis, Aaron M., Morgan, Richard G., McIntyre, Tim and Jacobs, Peter A. (2008). Nonequilibrium radiation intensity measurements in simulated Titan atmospheres. 26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference 2008, Seattle, United States, 23-26 June 2008. Reston, VA, United States: American Institute for Aeronautics and Astronautics (AIAA). doi: 10.2514/6.2008-4136

Nonequilibrium radiation intensity measurements in simulated Titan atmospheres

2008

Conference Publication

Simulation of radiating CO2–N2 shock layer experiments at hyperbolic entry conditions

Potter, Daniel F., Eichmann, Troy, Brandis, Aaron, Morgan, Richard G., Jacobs, Peter A. and McIntyre, Tim J. (2008). Simulation of radiating CO2–N2 shock layer experiments at hyperbolic entry conditions. 40th Thermophysics Conference, Seattle, Washington State, USA, 23-26 June 2008. Reston, Virigina: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2008-3933

Simulation of radiating CO2–N2 shock layer experiments at hyperbolic entry conditions

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