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2019 Conference Publication Testing a full-scale Hayabusa Model in a large expansion tubeAndrianatos, Andreas, Gildfind, David and Morgan, Richard (2019). Testing a full-scale Hayabusa Model in a large expansion tube. Asia Pacific International Symposium on Aerospace Technology (APISAT 2019), Gold Coast, QLD, Australia, 4-6 December 2019. |
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2019 Conference Publication Generating high speed earth re-entry test conditions in an expansion tubeJames, Christopher, Lewis, Steven, Gildfind, David, Morgan, Richard and McIntyre, Timothy (2019). Generating high speed earth re-entry test conditions in an expansion tube. 8th International Workshop on Radiation of High Temperature Gases, Madrid, Spain, 25-29 March 2019. |
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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 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. |
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2019 Conference Publication Generating High Speed Earth Re-entry Test Conditions in an Expansion Tube for Interplanetary Return MissionsJames, Christopher M., Lewis, Steven W., Gildfind, David E., Morgan, Richard G., McIntyre, Timothy J. and Liu, Yu (2019). Generating High Speed Earth Re-entry Test Conditions in an Expansion Tube for Interplanetary Return Missions. 32nd International Symposium on Shock Waves (ISSW32 2019), Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0424-cd |
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2019 Conference Publication Multidimensional effects and self- absorption on spectroscopic observations of Saturn entry radiationLiu, Yu, Toniato, Pierpaolo, James, Chris, Morgan, Richard and McIntyre, T.J. (2019). Multidimensional effects and self- absorption on spectroscopic observations of Saturn entry radiation. 11th Asia-Pacific International Symposium on Aerospace Technology, Gold Coast, Australia, 4-6 December 2019. Gold Coast, Australia: Engineers Australia. |
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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 Hypervelocity boundary-layer flow with high-temperature surface ablationTemme, Nils, James, Christopher M., McIntyre, Timothy, Lewis, Steven W. and Morgan, Richard G. (2019). Hypervelocity boundary-layer flow with high-temperature surface ablation. AIAA Aviation 2019 Forum, Dallas, TX United States, 17-21 June 2019. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3135 |
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2019 Conference Publication The X3R reflected shock tunnel: a new, long-duration operating mode for the X3 expansion tubeStennett, S. J., Gildfind, D. E., Jacobs, P. A., Morgan, R. G., James, C. M. and Toniato, P. (2019). The X3R reflected shock tunnel: a new, long-duration operating mode for the X3 expansion tube. Asia Pacific International Symposium on Aerospace Technology (APISAT 2019), Gold Coast, QLD, Australia, 4-6 December 2019. |
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2019 Book Chapter Experimental investigation of meteorites: ground test facilitiesLaux, Christophe O., MacDonald, Megan E., Jacobs, Carolyn, Mariotto, Pierre, Tibere-Inglesse, Augustin, McGuire, Sean D., Zander, Fabian, Morgan, Richard, Savino, Luigi, De Cesare, Mario, Ceglia, Giuseppe, Del Vecchio, Antonio, Paganucci, Fabrizio and D'Orazio, Massimo (2019). Experimental investigation of meteorites: ground test facilities. Hypersonic meteoroid entry physics. (pp. 11-1-11-41) edited by Gianpiero Colonna, Mario Capitelli and Annarita Laricchiuta. Bristol, United Kingdom: IOP Publishing. doi: 10.1088/2053-2563/aae894ch11 |
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2019 Conference Publication Optimisation and design of a fully instrumented Mach 12 nozzle for the X3 expansion tubeToniato, Pierpaolo, Gildfind, David, Jacobs, Peter A. and Morgan, Richard G. (2019). Optimisation and design of a fully instrumented Mach 12 nozzle for the X3 expansion tube. 31th International Symposium on Shock Waves, Nagoya, Japan, 9-14 July 2017. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-91017-8_108 |
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2019 Conference Publication Commissioning of the T6 Stalker TunnelCollen, Peter L., Doherty, Luke, McGilvray, Matthew, Naved, Imran, Penty Geraets, Rowland T., Hermann, Tobias A., Morgan, Richard G. and Gildfind, David (2019). Commissioning of the T6 Stalker Tunnel. AIAA Scitech 2019 Forum, San Diego, CA, United States, 7-11 January 2019. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-1941 |
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2019 Conference Publication Expansion tube experiments of graphite ablation and radiation in hypervelocity earth-entry flowsRavichandran, R., Lewis, S.W., James, C.M., Morgan, R.G. and McIntyre, T.J. (2019). Expansion tube experiments of graphite ablation and radiation in hypervelocity earth-entry flows. 8th International Workshop on Radiation of High Temperature Gases, Madrid, Spain, 25-29 March 2019. |
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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 Driver condition development for high enthalpy operation of the X3 expansion tubeAndrianatos, Andreas, Gildfind, David and Morgan, Richard G. (2019). Driver condition development for high enthalpy operation of the X3 expansion tube. 31st International Symposium on Shock Waves, Nagoya, Japan, 9-14 July 2017. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-91017-8_37 |
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2018 Journal Article Improved test time evaluation in an expansion tubeJames, Christopher M., Cullen, Timothy G. , Wei, Han, Lewis, Steven W., Gu, Sangdi, Morgan, Richard G. and McIntyre, Timothy J. (2018). Improved test time evaluation in an expansion tube. Experiments in Fluids, 59 (5) 87. doi: 10.1007/s00348-018-2540-1 |
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2018 Journal Article Implementation of a state-to-state analytical framework for the calculation of expansion tube flow propertiesJames, C. M., Gildfind, D. E., Lewis, S. W., Morgan, R. G. and Zander, F. (2018). Implementation of a state-to-state analytical framework for the calculation of expansion tube flow properties. Shock Waves, 28 (2), 349-377. doi: 10.1007/s00193-017-0763-3 |
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2018 Conference Publication Performance optimization of X3R: A new reflected shock tunnel mode for the X3 expansion tubeStennett, Samuel J., Gildfind, David E., Jacobs, Peter A. and Morgan, Richard G. (2018). Performance optimization of X3R: A new reflected shock tunnel mode for the X3 expansion tube. 34th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-3563 |
