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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 Hypersonics Research in AustraliaMorgan, Richard (2015). Hypersonics Research in Australia. Air Force Office of Scientific Research, Arlington, VA, United States, 25 March 2015. |
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2015 Conference Publication Shock tube simulation of low Mach number blast wavesMorgan, R. G. and Gildfind, D. E. (2015). Shock tube simulation of low Mach number blast waves. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_11 |
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2015 Conference Publication Shock standoff on hemi-spherical bodies in hypervelocity flowsZander, F., Jacobs, P. A., Gollan, R. J. and Morgan, R. G. (2015). Shock standoff on hemi-spherical bodies in hypervelocity flows. International Symposium on Shock Waves (ISSW29), Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_85 |
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2015 Conference Publication Radiative heat transfer measurements in low-density titan atmospheresJacobs, C. M., McIntyre, T. J., Morgan, R. G., Brandis, A. M. and Laux, C. O. (2015). Radiative heat transfer measurements in low-density titan atmospheres. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24–28 September 2012. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.T4519 |
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2015 Journal Article Measurements of Air Plasma/Ablator Interactions in an Inductively Coupled Plasma TorchMacDonald, Megan E., Jacobs, Carolyn M., Laux, Christophe O., Zander, Fabian and Morgan, Richard G. (2015). Measurements of Air Plasma/Ablator Interactions in an Inductively Coupled Plasma Torch. Journal of Thermophysics and Heat Transfer, 29 (1), 12-23. doi: 10.2514/1.T4402 |
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2015 Conference Publication Scaled earth re-entry experiments in the X2 expansion tubeFahy, Elise , Buttsworth, David and Morgan, Richard (2015). Scaled earth re-entry experiments in the X2 expansion tube. Asia-Pacific International Symposium on Aerospace Technology, Cairns, QLD, Australia, 25 -27 November 2015. |
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2015 Conference Publication Radiative heatflux measurements for Titan atmospheric entry condition in superorbital expansion tunnelPorat, Hadas and Morgan, Richard (2015). Radiative heatflux measurements for Titan atmospheric entry condition in superorbital expansion tunnel. International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. |
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2015 Conference Publication T6: The Oxford University Stalker TunnelMcGilvray, Matthew , Doherty, Luke , Morgan, Richard G. and Gildfind, David (2015). T6: The Oxford University Stalker Tunnel. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2-6 March 2015. |
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2015 Conference Publication Design and commissioning of a new lightweight piston for the X3 Expansion TubeGildfind, D. E., Morgan, R. G. and Sancho, J. (2015). Design and commissioning of a new lightweight piston for the X3 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_57 |
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2015 Conference Publication High Mach Number Scramjet Test Flows in the X3 Expansion TubeGildfind, D. E., Sancho Ponce, J. and Morgan, R. G. (2015). High Mach Number Scramjet Test Flows in the X3 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_58 |
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2015 Conference Publication T6: The Oxford University Stalker TunnelMcGilvray, Matthew, Doherty, Luke, Morgan, Richard G. and Gildfind, David E. (2015). T6: The Oxford University Stalker Tunnel. International Space Planes and Hypersonic Systems and Technologies Conferences, Glasgow, Scotland, 6-9 July 2015. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3545 |
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2015 Conference Publication Duplication of atmospheric entry in laboratories: what are radiatively coupled flows?Morgan, Richard (2015). Duplication of atmospheric entry in laboratories: what are radiatively coupled flows?. International Planetary Probe Workshop, Cologne, Germany, 15-19 June 2015. |
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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 |
