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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 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 Journal Article A compact shock-assisted free-piston driver for impulse facilitiesKendall, MA, Morgan, RG and Jacobs, PA (1997). A compact shock-assisted free-piston driver for impulse facilities. Shock Waves, 7 (4), 219-230. doi: 10.1007/s001930050078 |
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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 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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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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1996 Journal Article Visualization and analysis of bow shocks in a superorbital expansion tubeWegener, M, McIntyre, T, Stalker, R and Morgan, R (1996). Visualization and analysis of bow shocks in a superorbital expansion tube. Aiaa Journal, 34 (10), 2200-2202. doi: 10.2514/3.13376 |
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1996 Journal Article Shock-Tunnel investigation of hypervelocity free shear layers in a planar ductButtsworth, DR and Morgan, RG (1996). Shock-Tunnel investigation of hypervelocity free shear layers in a planar duct. Journal of Propulsion and Power, 12 (5), 998-1001. doi: 10.2514/3.24134 |
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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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1995 Journal Article A Gun Tunnel Investigation of Hypersonic Free Shear Layers in a Planar DuctButtsworth, DR, Morgan, RG and Jones, TV (1995). A Gun Tunnel Investigation of Hypersonic Free Shear Layers in a Planar Duct. Journal of Fluid Mechanics, 299 (-1), 133-152. doi: 10.1017/S0022112095003454 |
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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 Journal Article The Superorbital Expansion Tube Concept, Experiment and AnalysisNeely, AJ and Morgan, RG (1994). The Superorbital Expansion Tube Concept, Experiment and Analysis. Aeronautical Journal, 98 (973), 97-105. doi: 10.1017/S0001924000050107 |
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1994 Journal Article Transition of Compressible High Enthalpy Boundary-Layer Flow Over a Flat-PlateHe, Y and Morgan, RG (1994). Transition of Compressible High Enthalpy Boundary-Layer Flow Over a Flat-Plate. Aeronautical Journal, 98 (972), 25-34. doi: 10.1017/S0001924000050181 |
