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2005 Conference Publication New gauge design to measure radiative heat transfer to a Titan aerocapture vehicle in expansion tubesCapra, BR, Morgan, RG and Leyland, P (2005). New gauge design to measure radiative heat transfer to a Titan aerocapture vehicle in expansion tubes. 5th European Symposium on Aerothermodynamics for Space Vehicles, Cologne, Germany, 8-11 November 2004. The Netherlands: ESA Publications. |
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2005 Conference Publication Nozzle development for an expansion tunnelScott, MP, Jacobs, PA and Morgan, RG (2005). Nozzle development for an expansion tunnel. 24th International Symposium on Shock Waves, Beijing Peoples R China, Jul 11-16, 2004. BERLIN: SPRINGER-VERLAG BERLIN. doi: 10.1007/978-3-540-27009-6_41 |
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2005 Conference Publication Real gas effects on flows over rearward-facing steps in high enthalpy flowsHayne, M. J., Gai, S. L., Mee, D. J. and Morgan, R. G. (2005). Real gas effects on flows over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. doi: 10.1007/978-3-540-27009-6_36 |
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2004 Journal Article Experimental expansion tube study of the flow over a toroidal balluteMcIntyre, T. J., Lourel, I., Eichmann, T. N., Morgan, R. G., Jacobs, P. A. and Bishop, A. I. (2004). Experimental expansion tube study of the flow over a toroidal ballute. Journal of Spacecraft And Rockets, 41 (5), 716-725. doi: 10.2514/1.13104 |
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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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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 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 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 Journal Article Rarefied, Superorbital Flows in an Expansion TubeWheatley, Vincent, Chiu, Sam Hsieh-Hsiang, Jacobs, Peter A., Macrossan, Michael N., Mee, David J. and Morgan, Richard G. (2004). Rarefied, Superorbital Flows in an Expansion Tube. International Journal for Numerical Methods for Heat and Fluid Flow, 14 (4), 512-537. doi: 10.1108/09615530410532277 |
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2004 Journal Article Effects of hydrogen-air non-equilibrium chemistry on the performance of a model scramjet thrust nozzleStalker, R. J., Truong, N. K., Morgan, R. G. and Paull, A. (2004). Effects of hydrogen-air non-equilibrium chemistry on the performance of a model scramjet thrust nozzle. Aeronautical Journal, 108 (November), 575-584. doi: 10.1017/S0001924000000403 |
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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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2003 Journal Article Rocketdyne hypersonic flow laboratory as high-performance expansion tube for scramjet testingStewart, BS, Morgan, RG and Jacobs, PA (2003). Rocketdyne hypersonic flow laboratory as high-performance expansion tube for scramjet testing. Journal of Propulsion And Power, 19 (1), 98-103. doi: 10.2514/2.6085 |
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2003 Journal Article Heat transfer and flow behind a step in high enthalpy superorbital flowHayne, MJ, Mee, DJ, Morgan, RG, Gai, SL and McIntyre, TJ (2003). Heat transfer and flow behind a step in high enthalpy superorbital flow. Aeronautical Journal, 107 (1073), 435-442. doi: 10.1017/s0001924000130040 |
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2003 Other Outputs Finite-rate chemistry simulations of the X2 expansion tubeStewart, B. S., Jacobs, P.A. and Morgan, R. G. (2003). Finite-rate chemistry simulations of the X2 expansion tube. St. Lucia: Div. of Mech. Eng., The Univ. of Qld.. |
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2003 Journal Article Generalized nonequilibrium binary scaling for shock standoff on hypersonic blunt bodiesInger, G. R., Higgins, C. and Morgan, R. (2003). Generalized nonequilibrium binary scaling for shock standoff on hypersonic blunt bodies. Journal of Thermophysics And Heat Transfer, 17 (1), 126-128. doi: 10.2514/2.6744 |
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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 Journal Article Aerodynamic experiment of high enthalpy expansion tubeShi, Hong-Hui, Wang, Tian-Jun and Morgan, Richard (2002). Aerodynamic experiment of high enthalpy expansion tube. Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 20 (4), 483-486. |
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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. |
