|
2017 Conference Publication A new sliding joint to accommodate recoil of a free-piston driven expansion tubeGildfind, David and Morgan, Richard G. (2017). A new sliding joint to accommodate recoil of a free-piston driven expansion tube. The 30th International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-44866-4_105 |
|
2017 Conference Publication Preliminary experimental investigation of air radiation in super-orbital expanding flowWei, H., Morgan, R. G., Sheikh, U. A., Jacobs, P. A., Gollan, R. J. and McIntyre, T. J. (2017). Preliminary experimental investigation of air radiation in super-orbital expanding flow. International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-44866-4_8 |
|
2017 Conference Publication Development of a fast-response calorimeter heat transfer gauge for hypersonic ground testingGeraets, Rowland T. Penty, McGilvray, Matthew, Doherty, Luke J., Morgan, Richard G., James, Christopher M., Vanyai, Tristan and Buttsworth, David R. (2017). Development of a fast-response calorimeter heat transfer gauge for hypersonic ground testing. 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, Colorado, 5-9 June 2017. American Institute of Aeronautics and Astronautics Inc, AIAA. |
|
2017 Conference Publication Development of a fast-response calorimeter gauge for hypersonic ground testingGeraets, Rowland T. Penty, McGilvray, Matthew, Doherty, Luke J., Morgan, Richard G., James, Christopher M., Vanyai, Tristan and Buttsworth, David R. (2017). Development of a fast-response calorimeter gauge for hypersonic ground testing. AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, CO, United States, 5-9 June 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautic. doi: 10.2514/6.2017-3238 |
|
2017 Conference Publication Experimental and numerical investigation of air radiation in superorbital expanding flowWei, Han, Morgan, Richard G., McIntyre, Timothy J., Brandis, Aaron M. and Johnston, Christopher O. (2017). Experimental and numerical investigation of air radiation in superorbital expanding flow. 47th AIAA Thermophysics Conference, Denver, CO, United States, 5 - 9 June 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-4531 |
|
2017 Conference Publication Simulating gas giant entry with increased helium diluent in an expansion tubeJames, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W. and McIntyre, T. M. (2017). Simulating gas giant entry with increased helium diluent in an expansion tube. 30th International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. Cham, Switzerland: Springer International Publishing. doi: 10.1007/978-3-319-44866-4_104 |
|
2017 Conference Publication Study of afterbody radiation during mars entry in an expansion tubeGu, Sangdi, Morgan, Richard G. and McIntyre, Timothy J. (2017). Study of afterbody radiation during mars entry in an expansion tube. 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, United States, 9 - 13 January 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-0212 |
|
2017 Conference Publication Experimentally simulating gas giant entry in an expansion tubeJames, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W. and McIntyre, Timothy J. (2017). Experimentally simulating gas giant entry in an expansion tube. 21st International Space Planes and Hypersonic Systems and Technologies Conference, Xiamen, China, 6 - 9 March 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-2152 |
|
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 |
|
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. |
|
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 |
|
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 |
|
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. |
|
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. |
|
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 |
|
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. |
|
2015 Conference Publication Measurements of radiating flow fields in the vacuum ultravioletSheikh, U. A., Jacobs, C., Laux, C. O., Morgan, R. G. and McIntyre, T. J. (2015). Measurements of radiating flow fields in the vacuum ultraviolet. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_104 |
|
2015 Conference Publication On the current limits of simulating gas giant entry flows in an expansion tubeJames, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W., Fahy, Elise J. and McIntyre, Timothy J. (2015). On the current limits of simulating gas giant entry flows in an expansion tube. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6 - 9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3501 |
|
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. |
|
2015 Conference Publication Advanced hypersonic vehicle component testing using pre-heated models and infrared scanningMorgan, R., Rees, B., Rutherford, J., Jefferey, M., Sollart, M., Morris, N., Basore, K., James, C., Wei, H., Gu, S., Lewis, S. and Landsberg, W. (2015). Advanced hypersonic vehicle component testing using pre-heated models and infrared scanning. 7th Asia-Pacific International Symposium on Aerospace Technology (APISAT), Cairns, QLD, Australia., 25-27 November, 2015. |
