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2005 Conference Publication Heat transfer measurements on the first experimental layer of the FIRE II reentry vehicle in expansion tubesCapra, B. R., Leyland, P. and Morgan, R. G. (2005). Heat transfer measurements on the first experimental layer of the FIRE II reentry vehicle in expansion tubes. 5th European Symposium on Aerothermodynamics for Space Vehicles, Cologne, Germany, 8-11 November 2004. The Nethelands: ESA Publications. |
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2005 Conference Publication Superorbital expansion tube operation: estimates of flow conditions via numerical simulationJacobs, P. A., Silvester, T. B., Morgan, R. G., Scott ,M .P., Gollan, R. J. and McIntyre, T. J. (2005). Superorbital expansion tube operation: estimates of flow conditions via numerical simulation. 43rd AIAA Aerospace Science Meeting and Exhibit, Reno, Nevada, United States, 10 - 13 January 2005. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2005-694 |
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2004 Conference Publication Skin friction measurements in a duct in the X3 superorbital expansion tubeSilvester, T. B., Morgan, R. G. and Jacobs, P. A. (2004). Skin friction measurements in a duct in the X3 superorbital expansion tube. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Florida, USA, 11-14 July 2004. USA: American Institute of Aeronautics and Astronautics Inc. doi: 10.2514/6.2004-3551 |
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2004 Conference Publication Subscale testing of the FIRE II vehicle in a superorbital expansion tubeCapra, B.R., Leyland, P. and Morgan, R.G. (2004). Subscale testing of the FIRE II vehicle in a superorbital expansion tube. 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, U.S.A., 5 - 8 January 2004. United States: American Institute of Aeronautics and Astronautics, AIAA. doi: 10.2514/6.2004-1298 |
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2004 Conference Publication Flow establishment over rearward-facing steps in high enthalpy flowsHayne, M. J., Mee, D. J., Gai, S. L., Stewart, B. S. and Morgan, R. G. (2004). Flow establishment over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. |
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2004 Conference Publication Computational hypervelocity aerodynamics of a caret waveriderSilvester, T. B. and Morgan, R. G. (2004). Computational hypervelocity aerodynamics of a caret waverider. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Florida, USA, 11-14 July 2004. USA: American Institute of Aeronautics and Astronautics Inc. |
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2004 Conference Publication Heat transfer measurements of the first experimental layer of the fire II reentry vehicle in expansion tubesCapra, BR, Morgan, RG and Leyland, W (2004). Heat transfer measurements of the first experimental layer of the fire II reentry vehicle in expansion tubes. 5th European Symposium on Aerothermodynamics for Space Vehicles, Cologne Germany, Nov 08-11, 2004. 2200 AG NOORDWIJK: ESA PUBLICATIONS DIVISION C/O ESTEC. |
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2003 Conference Publication Studies on caret wings at super orbital speedsRamesh R., Kuhn M., Abdel Jawad M.M. and Morgan R.G. (2003). Studies on caret wings at super orbital speeds. 41st Aerospace Sciences Meeting and Exhibit 2003, Reno, NV, January 6, 2003-January 9, 2003. doi: 10.2514/6.2003-910 |
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2002 Conference Publication Shock standoff on hypersonic blunt bodies in multitemperature ionizing nonequilibrium gas flowsHiggins, Charlotte, Inger, George R., Morgan, Richard, Eichmann, Troy and McIntyre, Tim (2002). Shock standoff on hypersonic blunt bodies in multitemperature ionizing nonequilibrium gas flows. AIAA/ASME Joint Thermophysics and Heat Transfer Conference, St. Louis, United States, 24-26 June 2002. |
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2002 Conference Publication Stability tests in superorbital expansion tubesAbdel-Jawad, M., Mee, D. J., Morgan, R. G. and Chiu, S.H. (2002). Stability tests in superorbital expansion tubes. 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 Experimental and numerical studies of flows about a Toroidal BalluteLourel, I., Eichmann, T. N., Isbister, S., Mcintyre, T. J., Houwing, A. F. P. and Morgan, R. G. (2002). Experimental and numerical studies of flows about a Toroidal Ballute. 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 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 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 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 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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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 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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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 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 |
