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2023 Conference Publication Experimental VUV shock layer radiation measurements for 13 and 14 km/s high speed earth re-entry conditionsLock, S., Liu, Y., Morgan, R., James, C. and McIntyre, T. (2023). Experimental VUV shock layer radiation measurements for 13 and 14 km/s high speed earth re-entry conditions. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023. |
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2023 Conference Publication Preliminary results for CO2 recombination for low velocity, high density mars aerocapture conditionsSingh, M., Liu, Y., James, C.M., Morgan, R.G., Temme, N. and McIntyre, T.J. (2023). Preliminary results for CO2 recombination for low velocity, high density mars aerocapture conditions. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023. |
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2023 Conference Publication Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in X3 Expansion TunnelKennedy, Aaron, Penty Geraets, Rowland T., James, Christopher M., Thompson, Matthew, Morgan, Richard G., Austin, Joanna M., Zander, Fabian and McGilvray, Matthew (2023). Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in X3 Expansion Tunnel. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0271 |
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2021 Conference Publication Self-absorption and electron number density measurements on Saturn entry radiationLiu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy (2021). Self-absorption and electron number density measurements on Saturn entry radiation. AIAA Scitech 2021 Forum, Virtual, 11–15 and 19–21 January 2021. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-0209 |
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2021 Conference Publication Infrared thermography on a biconic model in Hypersonic expansion tube flowsCullen, Timothy G., James, Christopher M., Ravichandran, Ranjith, Thompson, Matthew, Moran, Michael, Ramesh, Ranjini, Morgan, Richard G. and Nadesan, Thirukumaran (2021). Infrared thermography on a biconic model in Hypersonic expansion tube flows. AIAA Scitech 2021 Forum, Virtual, 11–15 and 19–21 January 2021. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-0873 |
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2021 Conference Publication Experimental methods for studying post shock relaxationApirana, Steve F., James, Christopher M., Lewis, Steven and Morgan, Richard G. (2021). Experimental methods for studying post shock relaxation. AIAA Scitech 2021 Forum, Virtual, 11–15 and 19–21 January 2021. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-0446 |
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2021 Conference Publication A generalised calibration procedure for performing infrared thermography in expansion tubesRamesh, Ranjini, Morgan, Richard G. and Mee, David J. (2021). A generalised calibration procedure for performing infrared thermography in expansion tubes. AIAA Aviation Forum, Virtual, 2-6 August 2021. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-2981 |
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2020 Conference Publication Using aerothermodynamic similarity to experimentally study nonequilibrium giant planet entryLiu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy J. (2020). Using aerothermodynamic similarity to experimentally study nonequilibrium giant planet entry. Joint Thermophysics and Heat Transfer Conference, Atlanta, GA, United States, 25-29 June 2018. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.a34713 |
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2020 Conference Publication The X3R Free-Piston Reflected Shock Tunnel: Australia's New Large-Scale, Long-Duration Hypersonic Testing CapabilityStennett, Samuel J., Gildfind, David, Jacobs, Peter, Morgan, Richard, James, Christopher and Toniato, Pierpaolo (2020). The X3R Free-Piston Reflected Shock Tunnel: Australia's New Large-Scale, Long-Duration Hypersonic Testing Capability. 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Montreal, Canada , March 10-12, 2020. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-2447 |
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2020 Conference Publication Development of a fast-response diamond calorimeter heat transfer gaugeGeraets, Rowland T. Penty, McGilvray, Matthew, Doherty, Luke J., Morgan, Richard G., James, Christopher M. and Buttsworth, David R. (2020). Development of a fast-response diamond calorimeter heat transfer gauge. 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, CO USA, 5-9 June 2017. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.t5688 |
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2020 Conference Publication Infrared thermography in expansion tubes for Martian entry flowsRamesh, Ranjini, Morgan, Richard, Ravichandran, Ranjith and Mee, David (2020). Infrared thermography in expansion tubes for Martian entry flows. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Montréal, Québec, Canada, 10-12 March 2020. Reston, Virginia: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-2415 |
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2020 Conference Publication Scaled Apollo Heating Testing in a Large Expansion TubeJames, Christopher M., Ravichandran, Ranjith, Smith, Daniel R., Cullen, Timothy G. and Morgan, Richard (2020). Scaled Apollo Heating Testing in a Large Expansion Tube. AIAA AVIATION 2020 FORUM , Virtual Event, 15-19 June 2020. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-3278 |
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2020 Conference Publication Simulating Uranus Entry in an Expansion TubeJames, Christopher M., Liu, Yu and Morgan, Richard (2020). Simulating Uranus Entry in an Expansion Tube. AIAA AVIATION 2020 FORUM , Virtual Event, 15-19 June 2020. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-3110 |
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2019 Conference Publication Testing of ultra fast response, durable co-axial thermocouples for high enthalpy impulse facilitiesJames, Christopher M., Birch, Byrenn, Smith, Daniel R., Cullen, Timothy G., Millard, Theodore, Vella, Samuel, Liu, Yu, Morgan, Richard G., Stern, Nathan and Buttsworth, David (2019). Testing of ultra fast response, durable co-axial thermocouples for high enthalpy impulse facilities. AIAA Aviation 2019 Forum, Dallas, TX USA, 17-21 June 2019. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3007 |
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2019 Conference Publication Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared ThermographyRamesh, Ranjini, Kelly, Rory, Cullen, Timothy G., Morgan, Richard G. and Mee, David J. (2019). Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared Thermography. AIAA Aviation 2019 Forum, Dallas, TX, United States, 17-21 June 2019. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3006 |
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2019 Conference Publication Application of Infrared Thermography in an Expansion TunnelCullen, T., James, C., Gollan, R. and Morgan, R. (2019). Application of Infrared Thermography in an Expansion Tunnel. In: Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019). 32nd International Symposium on Shock Waves (ISSW32 2019), Singapore, (1139-1165). 14-19 July 2019. doi:10.3850/978-981-11-2730-4_0271-cd |
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2019 Conference Publication Evaluation of electrically insulating coatings for magnetohydrodynamic aerobraking experimentationGildfind, David, Smith, Daniel, Thompson, Owen, Jacobs, Peter, Morgan, Richard, Kelly, Rory and McIntyre, Tim (2019). Evaluation of electrically insulating coatings for magnetohydrodynamic aerobraking experimentation. 32nd International Symposium on Shock Waves (ISSW32), Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0014-cd |
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2019 Conference Publication Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnelCullen, 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. 31st International Symposium on Shock Waves, Nagoya, Japan, 9-14 July 2017. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-91017-8_24 |
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2019 Conference Publication Generating 5-km/s low density hypersonic test flows in an expansion tube for studying ultraviolet radiationThompson, Matthew, James, Christopher M., Lewis, Steven W., Gildfind, David E. and Morgan, Richard G. (2019). Generating 5-km/s low density hypersonic test flows in an expansion tube for studying ultraviolet radiation. 32nd International Symposium on Shock Waves, Singapore, 14-19 July 2019. Singapore: ISSW. doi: 10.3850/978-981-11-2730-4_0337-cd |
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2019 Conference Publication Development of a high enthalpy driver in an expansion tube for generating Uranus entry flow conditionsThompson, M., James, C.M. and Morgan, R.G. (2019). Development of a high enthalpy driver in an expansion tube for generating Uranus entry flow conditions. 11th Asia-Pacific International Symposium on Aerospace Technology, Gold Coast, Australia, 4-6 December 2019. Gold Coast, Australia: Engineers Australia. |
