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2006 Conference Publication Radiative and total heat transfer measurements to a Titan Explorer ModelCapra, B. R. and Morgan, R G (2006). Radiative and total heat transfer measurements to a Titan Explorer Model. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, ACT, Australia, 6-9 November 2006. U.S.A.: American Institute of Aeronautics and Astronautics. |
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2006 Conference Publication Expansion tube operating conditions for studying nonequilibrium radiation relevant to Titan AerocaptureBrandis, A. M., Gollan, R. J., Scott, M. P., Morgan, R. G. and Jacobs, P. A. (2006). Expansion tube operating conditions for studying nonequilibrium radiation relevant to Titan Aerocapture. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, California, USA, 9-12 July 2006. USA: American Institute of Aeronautics and Astronautics. |
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2005 Journal Article Scramjets and Shock Tunnels: The Queensland ExperienceStalker, R. J., Paull, A., Mee, D. J., Morgan, R. G. and Jacobs, P. A. (2005). Scramjets and Shock Tunnels: The Queensland Experience. Progress in Aerospace Sciences, 41 (6), 471-513. doi: 10.1016/j.paerosci.2005.08.002 |
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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 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 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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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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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 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 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 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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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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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. |
