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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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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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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 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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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 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 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 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 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 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 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 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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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. |
