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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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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 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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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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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 |
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2017 Journal Article Earth reentry flow over a phenolic aeroshell in the X2 expansion tubeBanerji, Nikhil, Leyland, Pénélope, Fahy, Elise and Morgan, Richard (2017). Earth reentry flow over a phenolic aeroshell in the X2 expansion tube. Journal of Thermophysics and Heat Transfer, 32 (2), 414-428. doi: 10.2514/1.T5255 |
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2017 Journal Article Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in X2Sheikh, Umar A., Wei, Han, Lewis, Steven W., James, Christopher M., Leyland, Pénélope, Morgan, Richard G. and McIntyre, Timothy J. (2017). Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in X2. AIAA Journal, 55 (12), 1-14. doi: 10.2514/1.J056021 |
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2017 Journal Article Venus entry flow over a decomposing aeroshell in X2 expansion tubeBanerji, Nikhil, Leyland, Pénélope, Fahy, Elise and Morgan, Richard G. (2017). Venus entry flow over a decomposing aeroshell in X2 expansion tube. Journal of Thermophysics and Heat Transfer, 32 (2), 1-11. doi: 10.2514/1.T5172 |
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2017 Journal Article Quantitative emission spectroscopy for superorbital reentry in expansion tube X2Hermann, Tobias, Lohle, Stefan, Bauder, Uwe, Morgan, Richard, Wei, Han and Fasoulas, Stefanos (2017). Quantitative emission spectroscopy for superorbital reentry in expansion tube X2. Journal of Thermophysics and Heat Transfer, 31 (2), 257-268. doi: 10.2514/1.T4898 |
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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 |
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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 |
