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2002 Conference Publication Transient force measurements at superorbital speedsAbdel-Jawad, M., Mee, D. J., Morgan, R. G., Jacobs, P.A. and Philpot, J.A. (2002). Transient force measurements at superorbital speeds. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23. |
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2002 Conference Publication A generalized nonequilibrium binary scaling for shock standoff on hypersonic blunt bodiesInger, G. R., Higgins, C. E. and Morgan, R. G. (2002). A generalized nonequilibrium binary scaling for shock standoff on hypersonic blunt bodies. 40th AIAA Aerospace Sciences Meeting, Reno, Nevada, USA, 14-17 January, 2002. USA: AIAA. doi: 10.2514/6.2002-1117 |
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2002 Journal Article Shock standoff on hypersonic blunt bodies in nonequilibrium gas flowsInger, GR, Higgins, C and Morgan, R (2002). Shock standoff on hypersonic blunt bodies in nonequilibrium gas flows. Journal of Thermophysics And Heat Transfer, 16 (2), 245-250. doi: 10.2514/2.6674 |
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2002 Conference Publication The starting processes of an expansion tube nozzleStewart, B. S., Jacobs, P.A. and Morgan, R. G. (2002). The starting processes of an expansion tube nozzle. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23. |
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2002 Conference Publication Sonic line location in reacting flowsMorgan, R. G., Abdel-Jawad, M. and Mee, D. J. (2002). Sonic line location in reacting flows. 40th AIAA Aerospace Sciences Meeting, Reno, Nevada, USA, 14-17 January, 2002. USA: AIAA. doi: 10.2514/6.2002-221 |
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2002 Conference Publication Sonic jump for planetary entry vehiclesAbdel-Jawad, M., Morgan, R. G. and Mee, D. J. (2002). Sonic jump for planetary entry vehicles. 11th AIAA/AAAF International Conference Space Planes and Hypersonic Systems and Technologies, Orleans, France, 29/09/02-04/10/02. USA: American Institute of Aeronautics and Astronautics. |
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2002 Conference Publication Heat transfer and flow behind a rearward facing step in a super-orbital expansion tubeHayne, M. J., Gai, S.L., Hillier, R., Morgan, R. G., Mee, D. J. and Mcintyre, T. J. (2002). Heat transfer and flow behind a rearward facing step in a super-orbital expansion tube. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23. |
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2002 Conference Publication The effect of dissociation on choking of ducted flowsLourel, I., Morgan, R. G. and McIntyre, T. J. (2002). The effect of dissociation on choking of ducted flows. 8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference 2002, St Louis, MO United States, 24-26 June 2002. Reston, Virigina: AIAA. doi: 10.2514/6.2002-2894 |
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2001 Book Chapter Free Piston-Driven Reflected Shock TunnelsMorgan, R. G. (2001). Free Piston-Driven Reflected Shock Tunnels. Handbook of Shock Waves. (pp. 587-601) edited by Gabi Ben-Dor, Ozer Igra and Tov Elperin. USA: Academic Press. |
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2001 Conference Publication Diagnostics of A Range of Highly Superorbital Carbon Dioxide FlowsWegener, Margaret, Sutcliffe, Mark, Morgan, Richard, McIntyre, Tim and Rubinsztein-Dunlop, Halina (2001). Diagnostics of A Range of Highly Superorbital Carbon Dioxide Flows. 39th AIAA Aeropspace Sciences Meeting and Exhibit, Reno, USA, 8-11 January, 2001. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2001-304 |
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2001 Journal Article The measurement of Pitot pressure in high enthalpy expansion tubesSutcliffe, MA and Morgan, RG (2001). The measurement of Pitot pressure in high enthalpy expansion tubes. Measurement Science & Technology, 12 (3), 327-334. doi: 10.1088/0957-0233/12/3/312 |
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2001 Conference Publication Establishment of test conditions in the RHYFL-X facilityStewart, B. S., Morgan, R. G., Jacobs, P.A., Austin, K.J. and Jenkins, D.M. (2001). Establishment of test conditions in the RHYFL-X facility. 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibition, Salt Lake City, Utah, USA, 8-11 July, 2001. USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2001-3678 |
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2001 Book Chapter Free piston-Driven expansion tubesMorgan, R. G. (2001). Free piston-Driven expansion tubes. Handbook of Shock Waves. (pp. 603-622) edited by Gabi Ben-Dor, Ozer Igra and Tov Elperin. San Diego CA USA: Academic Press. |
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2001 Conference Publication Heat transfer behind a step in high enthalpy super-orbital flowGai, S.L., Hayne, M. J., Gardner, A., Morgan, R. G. and Mee, D. J. (2001). Heat transfer behind a step in high enthalpy super-orbital flow. 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 8-11 January, 2001. USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2001-509 |
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2000 Journal Article Optical study of a light diaphragm rupture process in an expansion tubeWegener, Margaret, Sutcliffe, Mark and Morgan, Richard (2000). Optical study of a light diaphragm rupture process in an expansion tube. Shock waves, 10 (3), 167-178. doi: 10.1007/s001930050003 |
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2000 Conference Publication Development of X3, A superorbital expansion tubeMorgan R.G. (2000). Development of X3, A superorbital expansion tube. 38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, January 10, 2000-January 13, 2000. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2000-558 |
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2000 Journal Article High-enthalpy expansion tube experiments with gas injectionSasoh, A, Morgan, RG, Littleton, BN, McIntyre, TJ and Bishop, AI (2000). High-enthalpy expansion tube experiments with gas injection. AIAA Journal, 38 (12), 2253-2259. doi: 10.2514/2.916 |
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2000 Conference Publication Simulated atmospheric entry ablation in superorbital flowsHunt D.C. and Morgan R.G. (2000). Simulated atmospheric entry ablation in superorbital flows. 38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United States, 10-13 January 2000. doi: 10.2514/6.2000-502 |
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2000 Conference Publication The RHYFL facility as a high performance expansion tube for scramjet testingStewart, B. S., Morgan, R. G., Jacobs, P. A. and Jenkins, D. (2000). The RHYFL facility as a high performance expansion tube for scramjet testing. 21st AIAA Aerodynamic Measurement Technology & Ground Testing, Denver, Colorado, USA, 19-22 June, 2000. Virginia, USA: AIAA. doi: 10.2514/6.2000-2595 |
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1999 Conference Publication Ionisation in hypervelocity flowsHerbrig, H. H., Morgan, R. G., Littleton, B. and McIntyre, T. J. (1999). Ionisation in hypervelocity flows. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton. |
