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2006 Conference Publication Impulse facility simulation of hypervelocity radiating flowsBrandis, A. M., Buttsworth, D. R., Capra, B. R., Eichmann, T., Gollan, R. J., Jacobs, C. M., Jacobs, P. A., Macrossan, M. N., McGilvray, M., McIntyre, T. J., Morgan, R. G., Potter, D. F., Scott, M. P. and van Diem, D. (2006). Impulse facility simulation of hypervelocity radiating flows. 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Rome, Italy, 6-8 September 2006. The Netherlands: ESA Publications. |
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2006 Conference Publication Radiation measurements in nonreflected shock tunnelsMorgan, Richard, Mcintyre, Tim, Gollan, Rowan, Jacobs, Peter, Brandis, Aaron, McGilvray, Matthew, Van Diem, Dwight, Gnoffo, Peter, Pulsonnetti, Maria V. and Wright, Michael (2006). Radiation measurements in nonreflected shock tunnels. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, CA, United States, 5-8 June 8 2006. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2006-2958 |
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2005 Conference Publication Geometrical Nozzle Design for Wagtail Rocket MotorsMcGilvray, Matthew, Teakle, Phillip, Jacobs, Peter and Morgan, Richard (2005). Geometrical Nozzle Design for Wagtail Rocket Motors. 5th Australian Space Science Conference, Melbourne (Hosted by RMIT), September 14 - 16, 2005. |
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2005 Conference Publication Flow establishment over rearward-facing steps in high enthalpy flowsHayne, MJ, Mee, DJ, Gai, SL, Stewart, BS and Morgan, RG (2005). Flow establishment over rearward-facing steps in high enthalpy flows. 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_23 |
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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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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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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 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 Operating conditions in UQ's impulse facilities for scramjet testingMcGilvray, M., Morgan, R. G., Paull, A., Abdel-Jawad, M. M., Jacobs, P. A., McIntyre, T. J. and Scott, M. A. (2005). Operating conditions in UQ's impulse facilities for scramjet testing. 25th International Symposium on Shock Waves, Bangalore, India, 17-22 July 2005. |
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2005 Conference Publication Expansion tube investigations of planetary aerodynamicsMorgan, Richard G. (2005). Expansion tube investigations of planetary aerodynamics. 25th International Symposium on Shock Waves – ISSW25, Bangalore, India, 17-22 July 2005. Hyderabad, A.P., India: Universities Press (India). |
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2005 Conference Publication A new single stage driver for the X2 expansion tubeScott, Michael P., Morgan, Richard G. and Jacobs, Peter A. (2005). A new single stage driver for the X2 expansion tube. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers, Reno, NV USA, 10-13 January 2005. doi: 10.2514/6.2005-697 |
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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 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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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 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 |
