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2001 Conference Publication Diagnostics of A Range of Highly Superorbital Carbon Dioxide FlowsWegener, Margaret, Sutcliffe, Mark, Morgan, Richard, McIntyre, Tim and Rubinsztein-Dunlop, Halina (2001). Diagnostics of A Range of Highly Superorbital Carbon Dioxide Flows. 39th AIAA Aeropspace Sciences Meeting and Exhibit, Reno, USA, 8-11 January, 2001. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2001-304 |
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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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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 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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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 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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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 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 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. |
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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 review of the use of expansion tubes for creating superorbital flowsMorgan R.G. (1997). A review of the use of expansion tubes for creating superorbital flows. 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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1996 Conference Publication A two stage free-piston driver for expansion tubesDoolan C.J. and Morgan R.G. (1996). A two stage free-piston driver for expansion tubes. 34th Aerospace Sciences Meeting and Exhibit, 1996, Reno, NV, January 15, 1996-January 18, 1996. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1996-854 |
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1996 Conference Publication A shock tunnel investigation of scramjet performance with partially premixed combustionStalker, R.J., Morgan, R.G. and Paull, A. (1996). A shock tunnel investigation of scramjet performance with partially premixed combustion. Space Plane and Hypersonic Systems and Technology Conference, 1996, *, 18-22 November 1996. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1996-4534 |
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1994 Conference Publication Martian atmospheric entry studies with chemical kinetics in an expansion tubeSutcliffe, M. A. and Morgan, R. G. (1994). Martian atmospheric entry studies with chemical kinetics in an expansion tube. IE Aust. |
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1994 Conference Publication High performance, compact free piston driver for shock tubes: practical considerationsKendall, M. A. and Morgan, R. G. (1994). High performance, compact free piston driver for shock tubes: practical considerations. Proceedings of the 9th National Space Engineering Symposium 1994, Kensington, NSW, Australia, 5-7 September 1994. Institution of Engineers. |
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1994 Conference Publication Scramjet combustion and thrust measurements in a reflected shock tunnel with varied test gas atomic oxygen contaminationBakos, R. J. and Morgan, R. G. (1994). Scramjet combustion and thrust measurements in a reflected shock tunnel with varied test gas atomic oxygen contamination. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1994-2520 |
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1994 Conference Publication Measurement of heating rates for earth entry at 13 kms-1Neely, A. J. and Morgan, R. G. (1994). Measurement of heating rates for earth entry at 13 kms-1 . AIAA 25th Plasmadynamics and Lasers Conference, 1994, Colorado Springs, CO, June 20, 1994-June 23, 1994. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1994-2606 |
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1994 Conference Publication Supersonic Combustion Experiments in Free-Piston Reflected Shock TunnelsMorgan, RG (1994). Supersonic Combustion Experiments in Free-Piston Reflected Shock Tunnels. Workshop on Combustion, Hampton Va, Oct 12-14, 1992. DORDRECHT: KLUWER ACADEMIC PUBL. |
