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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 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 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. |
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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 Journal Article Chemical recombination in an expansion tubeBakos Robert J. and Morgan Richard G. (1994). Chemical recombination in an expansion tube. AIAA journal, 32 (6), 1316-1319. doi: 10.2514/3.12135 |
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1993 Journal Article Numerical Modeling of Wall-Injected Scramjet ExperimentsBrescianini, CP and Morgan, RG (1993). Numerical Modeling of Wall-Injected Scramjet Experiments. Journal of Propulsion and Power, 9 (2), 169-175. doi: 10.2514/3.23605 |
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1993 Conference Publication Expansion Tube Simulation of Martian Hypervelocity AerodynamicsSutcliffe, MA, Morgan, RG and Neely, AJ (1993). Expansion Tube Simulation of Martian Hypervelocity Aerodynamics. 8th National Space Engineering Symposium, St Lucia Australia, Sep 20-21, 1993. BARTON: INST ENGINEERS AUSTRALIA. |
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1993 Conference Publication Test-Time Optimization of a Large-Scale Hypervelocity Expansion TunnelDoolan, CJ and Morgan, RG (1993). Test-Time Optimization of a Large-Scale Hypervelocity Expansion Tunnel. 8th National Space Engineering Symposium, St Lucia Australia, Sep 20-21, 1993. BARTON: INST ENGINEERS AUSTRALIA. |
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1993 Conference Publication Pushing the Edge of the Groundtesting Envelope - the Superorbital Expansion TubeNeely, AJ and Morgan, RG (1993). Pushing the Edge of the Groundtesting Envelope - the Superorbital Expansion Tube. 8th National Space Engineering Symposium, St Lucia Australia, Sep 20-21, 1993. BARTON: INST ENGINEERS AUSTRALIA. |
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1993 Conference Publication Nonisentropic Shock Tunnel Driver ConceptsKendall, MA and Morgan, RG (1993). Nonisentropic Shock Tunnel Driver Concepts. 8th National Space Engineering Symposium, St Lucia Australia, Sep 20-21, 1993. BARTON: INST ENGINEERS AUSTRALIA. |
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1992 Conference Publication Flow Measurements and Calibration of a Superorbital Expansion TubeNeely, AJ and Morgan, RG (1992). Flow Measurements and Calibration of a Superorbital Expansion Tube. 11th Australasian Fluid Mechanics Conference, Hobart Australia, Dec 14-18, 1992. HOBART: UNIVERSITY TASMANIA. |
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1992 Conference Publication Effects of oxygen dissociation on hypcrvelocity combustion experimentsBakos, R. J., Morgan, R. G. and Tamagno, J. (1992). Effects of oxygen dissociation on hypcrvelocity combustion experiments. AIAA/ASME/SAE/ASEE 28th Joint Propulsion Conference and Exhibit, 1992, Nashville, TN, July 6, 1992-July 8, 1992. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1992-3964 |
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1992 Conference Publication An investigation of a wall-injected scramjet using a shock tunnelBrescianini, C. P. and Morgan, R. G. (1992). An investigation of a wall-injected scramjet using a shock tunnel. AIAA/ASME/SAE/ASEE 28th Joint Propulsion Conference and Exhibit, 1992, Nashville, TN, United States, 6-8 July 1992. Reston, VA, United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1992-3965 |
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1992 Conference Publication Axisymmetric Scramjet Thrust ProductionBakos, RJ and Morgan, RG (1992). Axisymmetric Scramjet Thrust Production. 11th Australasian Fluid Mechanics Conference, Hobart Australia, Dec 14-18, 1992. HOBART: UNIVERSITY TASMANIA. |
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1992 Conference Publication A Compound Isentropic Free Piston Driver for Expansion TunnelsMorgan, RG (1992). A Compound Isentropic Free Piston Driver for Expansion Tunnels. 11th Australasian Fluid Mechanics Conference, Hobart Australia, Dec 14-18, 1992. HOBART: UNIVERSITY TASMANIA. |
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1992 Conference Publication Shock Interactions with Hypersonic Mixing Layers - Steady Flow Analysis and ExperimentsButtsworth, DR and Morgan, RG (1992). Shock Interactions with Hypersonic Mixing Layers - Steady Flow Analysis and Experiments. 11th Australasian Fluid Mechanics Conference, Hobart Australia, Dec 14-18, 1992. HOBART: UNIVERSITY TASMANIA. |
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1988 Journal Article Wave Processes in Scramjet Thrust GenerationStalker, RJ, Morgan, RG and Netterfield, MP (1988). Wave Processes in Scramjet Thrust Generation. Combustion and Flame, 71 (1), 63-77. doi: 10.1016/0010-2180(88)90106-X |
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1987 Journal Article HYDROGEN SCRAMJET WITH SIDE WALL INJECTIONMorgan, R. G., Paull, A., Morris, N. A. and Stalker, R. J. (1987). HYDROGEN SCRAMJET WITH SIDE WALL INJECTION. Trans Inst ENG Aust Multi Discip Eng, GEll (1), 45-51. |
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1987 Conference Publication Silane as an ignition aid in scramjetsMorris, N. A., Morgan, R. G., Paull, A. and Stalker, R. J. (1987). Silane as an ignition aid in scramjets. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1987-1636 |
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1986 Journal Article Shock Tunnel Measurements of Heat-Transfer in a Model ScramjetMorgan, RG and Stalker, RJ (1986). Shock Tunnel Measurements of Heat-Transfer in a Model Scramjet. Journal of Spacecraft and Rockets, 23 (5), 470-475. doi: 10.2514/3.25831 |
