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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 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 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 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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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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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 |
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2018 Conference Publication Improving high enthalpy expansion tube condition characterisation using high speed imageryJames, Christopher M., Smith, Daniel R., McLean, Carl, Morgan, Richard G., Lewis, Steven W. and Toniato, Pierpaolo (2018). Improving high enthalpy expansion tube condition characterisation using high speed imagery. 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 Inc, AIAA. doi: 10.2514/6.2018-3805 |
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2018 Conference Publication Experimental analysis of the interaction of carbon and silicon ablation products with expanding hypersonic flowsDonegan, Brian E., Greendyke, Robert B., Ravichandran, Ranjith, Lewis, Steven W., Morgan, Richard G., McIntyre, Timothy J. and Apostolov, Zlatomir D. (2018). Experimental analysis of the interaction of carbon and silicon ablation products with expanding hypersonic flows. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018, Orlando, FL, United States, 17-19 September 2018. Reston, VA, United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2018-5325 |
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2018 Conference Publication Flow characterization and modeling of the X2 and X3 expansion tubesGildfind, David E., Jacobs, Peter A., Gollan, Rowan J., Toniato, Pierpaolo, McIntyre, Timothy J., Andrianatos, Andreas, James, Christopher M. and Morgan, Richard G. (2018). Flow characterization and modeling of the X2 and X3 expansion tubes. VKI Lecture Series STO-AVT-235 on Flow Characterization and Modeling of Hypersonic Wind Tunnels, Brussels, Belgium, 3-5 December 2018. |
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2018 Conference Publication Full free-stream mach 12 scramjet testing in expansion tubesToniato, Pierpaolo, Gildfind, David E., Andrianatos, Andreas and Morgan, Richard G. (2018). Full free-stream mach 12 scramjet testing in expansion tubes. 36th AIAA Applied Aerodynamics Conference, 2018, Atlanta, GA United States, 25-29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-3818 |
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2018 Conference Publication Rapid prototyping in instrumented hypervelocity testingEldridge, R., James, C.M., Apirana, S. and Morgan, R.G. (2018). Rapid prototyping in instrumented hypervelocity testing. 18th Australian Space Research Conference, Gold Coast, QLD, Australia, 24-26 September 2018. |
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2018 Conference Publication Experimental study of saturn entry radiation with higher amount of diluent in an expansion tubeLiu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy J. (2018). Experimental study of saturn entry radiation with higher amount of diluent in an expansion tube. 12th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-4070 |
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2017 Journal Article Experimental evidence of the impact of radiation coupling on binary scaling applied to shock layer flowsde Crombrugghe, G., Chazot, O., McIntyre, T. J. and Morgan, R. (2017). Experimental evidence of the impact of radiation coupling on binary scaling applied to shock layer flows. International Journal of Heat and Mass Transfer, 120, 568-574. doi: 10.1016/j.ijheatmasstransfer.2017.12.071 |
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2017 Journal Article Scramjet test flow reconstruction for a large-scale expansion tube, part 1: quasi-one-dimensional modellingGildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. K. and Gollan, R. J. (2017). Scramjet test flow reconstruction for a large-scale expansion tube, part 1: quasi-one-dimensional modelling. Shock Waves, 28 (4), 1-21. doi: 10.1007/s00193-017-0785-x |
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2017 Journal Article Scramjet test flow reconstruction for a large-scale expansion tube, Part 2: axisymmetric CFD analysisGildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. C. and Gollan, R. J. (2017). Scramjet test flow reconstruction for a large-scale expansion tube, Part 2: axisymmetric CFD analysis. Shock Waves, 28 (4), 1-20. doi: 10.1007/s00193-017-0786-9 |
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2017 Journal Article Carbon ablation in hypervelocity air and nitrogen shock layersLewis, Steven W., James, Christopher M., Ravichandran, Ranjith, Morgan, Richard G. and McIntyre, Timothy J. (2017). Carbon ablation in hypervelocity air and nitrogen shock layers. Journal of Thermophysics and Heat Transfer, 32 (2), 449-468. doi: 10.2514/1.T5270 |
