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2016 Journal Article Numerical modeling of Earth reentry flow with surface ablationAlba, Christopher R., Greendyke, Robert B., Lewis, Steven W., Morgan, Richard G. and McIntyre, Timothy J. (2016). Numerical modeling of Earth reentry flow with surface ablation. Journal of Spacecraft and Rockets, 53 (1), 84-97. doi: 10.2514/1.A33266 |
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2016 Conference Publication Experimental and computational fluid dynamics studies of superorbital earth re-entryFahy, Elise J., Gollan, Rowan J., Buttsworth, David R., Jacobs, Peter A. and Morgan, Richard G. (2016). Experimental and computational fluid dynamics studies of superorbital earth re-entry. 46th AIAA Thermophysics Conference, Washington, DC, United States, 13 - 17 June 2016. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-3532 |
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2016 Book Chapter Expansion tubes in AustraliaGildfind, David, Morgan, Richard G. and Jacobs, Peter A. (2016). Expansion tubes in Australia. Experimental methods of shock wave research. (pp. 399-431) edited by Ozer Igra and Friech Seiler. Basel, Switzerland: Springer. doi: 10.1007/978-3-319-23745-9_13 |
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2016 Conference Publication Current progress of the development of a Mach 12 scramjet operating condition in the X3 expansion tubeToniato, Pierpaolo, Gildfind, David and Morgan, Richard G. (2016). Current progress of the development of a Mach 12 scramjet operating condition in the X3 expansion tube. 11th International Workshop on Shock Tube Technology, Gottingen, Germany, 30 June -2 July 2016. |
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2016 Conference Publication Analysis and rebuilding of experiments on a heated carbon graphite model in the X2 expansion tubeMora-Monteros, Jérémy, Leyland, Pénélope, Hannema, Gwenael, Sheikh, Umar, Fahy, Elise, Morgan, Richard G. and Morgan, Timothy J. (2016). Analysis and rebuilding of experiments on a heated carbon graphite model in the X2 expansion tube. 46th AIAA Thermophysics Conference, Washington, DC, United States, 13 - 17 June 2016. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-4155 |
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2016 Conference Publication Development of a new Mach 12 scramjet operating capability in the X3 expansion tubeToniato, Pierpaolo, Gildfind, David E., Jacobs, Peter A. and Morgan, Richard G. (2016). Development of a new Mach 12 scramjet operating capability in the X3 expansion tube. Asia-Pacific International Symposium on Aerospace Technology (APISAT), Cairns, QLD, Australia, 25 – 27 November 2015. |
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2016 Conference Publication Expansion tunnel ablation testing in venus entry conditionBanerji, Nikhil, Leyland, Pénélope and Morgan, Richard G. (2016). Expansion tunnel ablation testing in venus entry condition. 46th AIAA Thermophysics Conference, Washington, DC, United States, 13 - 17 June 2016. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-3231 |
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2016 Conference Publication Preliminary development of high enthalpy conditions for the X3 expansion tubeAndrianatos, A., Gildfind, D. and Morgan, R. (2016). Preliminary development of high enthalpy conditions for the X3 expansion tube. 20th Australasian Fluid Mechanics Conference, 20AFMC, Perth, WA, Australia, 5-8 December 2016. Australasian Fluid Mechanics Society. |
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2016 Conference Publication The ESA ARC project: Ablation radiation coupling for hypervelocity re-entry with low density type ablatorsLeyland, Pénélope, Sheikh, Umar, Duval, Basil, Hermann, Tobias, Loehle, Stefan, McIntyre, Timothy J., Morgan, Richard, Wei, Han, Bouilly, Jean-Marc and Marraffa, Lionel (2016). The ESA ARC project: Ablation radiation coupling for hypervelocity re-entry with low density type ablators. 46th AIAA Thermophysics Conference 2016, Washington, DC United States, 13-17 June 2016. Reston, VA United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2016-3234 |
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2016 Conference Publication Extension of the X3 expansion tube capabilities for Mach 12 scramjet testing: flow condition: development and nozzle optimizationToniato, P., Gildfind, D. E., Jacobs, P. A. and Morgan, R. G. (2016). Extension of the X3 expansion tube capabilities for Mach 12 scramjet testing: flow condition: development and nozzle optimization. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, Australia, 5-8 December 2-16. Perth, Australia: Australasian Fluid Mechanics Society. |
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2015 Journal Article A new sliding joint to accommodate recoil of a free-piston-driven expansion tube facilityGildfind, D.E. and Morgan, Richard G. (2015). A new sliding joint to accommodate recoil of a free-piston-driven expansion tube facility. Shock Waves Journal, 26 (6), 825-833. doi: 10.1007/s00193-015-0609-9 |
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2015 Journal Article Vacuum ultraviolet spectral measurements for superorbital earth entry in X2 expansion tubeSheikh, Umar A., Morgan, Richard G. and McIntyre, Timothy J. (2015). Vacuum ultraviolet spectral measurements for superorbital earth entry in X2 expansion tube. AIAA Journal, 53 (12), 3589-3602. doi: 10.2514/1.J054027 |
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2015 Journal Article Performance considerations for expansion tube operation with a shock-heated secondary driverGildfind, David E., James, Chris M., Toniato, Pierpaolo and Morgan, Richard G. (2015). Performance considerations for expansion tube operation with a shock-heated secondary driver. Journal of Fluid Mechanics, 777, 364-407. doi: 10.1017/jfm.2015.349 |
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2015 Journal Article Free-piston driver performance characterisation using experimental shock speeds through heliumGildfind, D. E., James, C. M. and Morgan, R. G. (2015). Free-piston driver performance characterisation using experimental shock speeds through helium. Shock Waves, 25 (2), 169-176. doi: 10.1007/s00193-015-0553-8 |
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2015 Conference Publication Emission spectroscopy of a mach disk at Titan atmospheric entry conditionsPorat, Hadas, Zander, Fabian, Morgan, Richard G. and McIntyre, Timothy J. (2015). Emission spectroscopy of a mach disk at Titan atmospheric entry conditions. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July, 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_94 |
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2015 Conference Publication Limits of Simulating Gas Giant Entry at True Gas Composition and True Flight Velocities in an Expansion TubeJames, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W., Fahy, E. J. and McIntyre, T.J. (2015). Limits of Simulating Gas Giant Entry at True Gas Composition and True Flight Velocities in an Expansion Tube. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2-6 March 2015. |
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2015 Conference Publication Transitional and Turbulent Heating in Re-Entry flow, Presentation to the meeting of NATO STO AVT-240 RTG-082 working group on Hypersonic TransitionMorgan, Richard (2015). Transitional and Turbulent Heating in Re-Entry flow, Presentation to the meeting of NATO STO AVT-240 RTG-082 working group on Hypersonic Transition. Hypersonic Transition, Tuscon, Arizona, 26-27 March 2015. |
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2015 Conference Publication Simulating gas giant entry in an expansion tubeJames, C., Gildfind, D., Morgan, R, Lewis, S., Fahy, E. and McIntyre, T. (2015). Simulating gas giant entry in an expansion tube. 7th Asia-Pacific International Symposium on Aerospace Technology, Cairns, Australia, 25-27 November 2015. |
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2015 Conference Publication Comparison of carbon ablative shock-layer radiation with high surface temperaturesLewis, Steven W., Morgan, Richard G., McIntyre, Timothy J., Alba, Christopher R. and Greendyke, Robert B. (2015). Comparison of carbon ablative shock-layer radiation with high surface temperatures. 45th AIAA Thermophysics Conference, Dallas, TX, United States, 22-26 June, 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-2348 |
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2015 Conference Publication Working towards simulating gas giant entry radiation in an expansion tubeJames, C .M., Gildfind, D. E., Morgan, R. G. and McIntyre, T. J. (2015). Working towards simulating gas giant entry radiation in an expansion tube. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_89 |
