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2001 Journal Article The measurement of Pitot pressure in high enthalpy expansion tubesSutcliffe, MA and Morgan, RG (2001). The measurement of Pitot pressure in high enthalpy expansion tubes. Measurement Science & Technology, 12 (3), 327-334. doi: 10.1088/0957-0233/12/3/312 |
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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. |
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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 |
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2000 Journal Article Optical study of a light diaphragm rupture process in an expansion tubeWegener, Margaret, Sutcliffe, Mark and Morgan, Richard (2000). Optical study of a light diaphragm rupture process in an expansion tube. Shock waves, 10 (3), 167-178. doi: 10.1007/s001930050003 |
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2000 Conference Publication The RHYFL facility as a high performance expansion tube for scramjet testingStewart, B. S., Morgan, R. G., Jacobs, P. A. and Jenkins, D. (2000). The RHYFL facility as a high performance expansion tube for scramjet testing. 21st AIAA Aerodynamic Measurement Technology & Ground Testing, Denver, Colorado, USA, 19-22 June, 2000. Virginia, USA: AIAA. doi: 10.2514/6.2000-2595 |
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2000 Conference Publication Development of X3, A superorbital expansion tubeMorgan R.G. (2000). Development of X3, A superorbital expansion tube. 38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, January 10, 2000-January 13, 2000. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2000-558 |
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2000 Journal Article High-enthalpy expansion tube experiments with gas injectionSasoh, A, Morgan, RG, Littleton, BN, McIntyre, TJ and Bishop, AI (2000). High-enthalpy expansion tube experiments with gas injection. AIAA Journal, 38 (12), 2253-2259. doi: 10.2514/2.916 |
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2000 Conference Publication Simulated atmospheric entry ablation in superorbital flowsHunt D.C. and Morgan R.G. (2000). Simulated atmospheric entry ablation in superorbital flows. 38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United States, 10-13 January 2000. doi: 10.2514/6.2000-502 |
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1999 Conference Publication Ionisation in hypervelocity flowsHerbrig, H. H., Morgan, R. G., Littleton, B. and McIntyre, T. J. (1999). Ionisation in hypervelocity flows. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton. |
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1999 Conference Publication Total radiative and convective heat transfer to re-entry bodies at superorbital velocitiesPalmer, R. and Morgan, R. G. (1999). Total radiative and convective heat transfer to re-entry bodies at superorbital velocities. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton. |
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1999 Journal Article A two-stage free piston driverDoolan, C. J. and Morgan, R. G. (1999). A two-stage free piston driver. Shock Waves, 9 (4), 239-248. doi: 10.1007/s001930050161 |
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1999 Conference Publication Simulation of ablative mixing layers in superorbital flowsMorgan, R. G., Sasoh, A., Littleton, B., Bishop, A., McIntyre, T. J., Hoogland, J. and Gardner, A. (1999). Simulation of ablative mixing layers in superorbital flows. 22nd International Symposium on Shock Waves, Imperial College, London, UK, 18-23 July, 1999. Southampton, UK: University of Southampton. |
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1998 Conference Publication The aerodynamic stability of superorbital reentry craftMorgan, R. G. and Stewart, B. S. (1998). The aerodynamic stability of superorbital reentry craft. Monash University. |
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1998 Journal Article Ballistic heating of propelling gas in a shock tube with a free-moving pistonShmelev, VM, Kendall, MA and Morgan, RG (1998). Ballistic heating of propelling gas in a shock tube with a free-moving piston. High Temperature, 36 (2), 299-304. |
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1997 Conference Publication Stagnation point heat transfer in superorbital expansion tubesPalmer R.A. and Morgan R.G. (1997). Stagnation point heat transfer in superorbital expansion tubes. 35th Aerospace Sciences Meeting and Exhibit, 1997, January 6, 1997-January 9, 1997. American Institute of Aeronautics and Astronautics Inc, AIAA. |
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1997 Conference Publication Mechanical and Space Engineering, a degree for undergraduatesMorgan R.G., Mee D.J. and Macrossan M.N. (1997). Mechanical and Space Engineering, a degree for undergraduates. 35th Aerospace Sciences Meeting and Exhibit, 1997, Reno, NV, United States, 6-9 January 1997. American Institute of Aeronautics and Astronautics Inc, AIAA. |
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1997 Conference Publication A study of free-piston driven double-diaphragm drivers for expansion tubesKendall, M. A., Morgan, R. G. and Petrie-Repar, P. J. (1997). A study of free-piston driven double-diaphragm drivers for expansion tubes. American Institute of Aeronautics and Astronautics Inc, AIAA. |
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1997 Journal Article Experiments on oblique shock interactions with planar mixing regionsButtsworth, D. R., Morgan, R. G. and Jones, T. V. (1997). Experiments on oblique shock interactions with planar mixing regions. AIAA Journal, 35 (11), 1774-1777. doi: 10.2514/2.26 |
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1997 Conference Publication Experimental and theoretical investigation of hypervelocity carbon dioxide flowsSutcliffe M.A. and Morgan R.G. (1997). Experimental and theoretical investigation of hypervelocity carbon dioxide flows. 35th Aerospace Sciences Meeting and Exhibit, 1997, Reno, NV, United States, 6-9 January 1997. American Institute of Aeronautics and Astronautics Inc, AIAA. |
