Professor Richard Morgan
Professor
School of Mechanical and Mining Engineering
+61 7 336 53592
Researcher biography
Prof Morgan was the Director of the Centre for Hypersonics since its inception in 1997 until October 2021. He lectures in mechanical and aerospace engineering within the School of Mechanical and Mining Engineering.
He has a strong research record in the development of hypervelocity impulsive facilities on which the UQ Centre for Hypersonics research program is based, including the ‘X’ series of super-orbital expansion tubes, and has extensive experience in hypersonic aero-thermo-dynamics and scramjet propulsion.
Richard Morgan has been developing superorbital ground based facilities for many years, and has collaborative research program with DSTG, NASA, ESA, Oxford University, Ecole Centrale (Paris) and AOARD in radiating flows, as well as continuing ARC support in this area since 1990, including two current ARC Discovery grants in partnership with European and American partners.
He was involved as a flight team member in the 2010 airborne observation of the Japanese ‘Hayabusa’ asteroid sample return mission, for which he was a co-recipient of the NASA Ames ‘honour’ award for 2010. He regularly gives invited talks in international meetings, and gave a plenary presentation to the AIAA Hypersonic Spaceplanes Conference in San Francisco in April 2011.
Professor Richard Morgan was awarded a 2012 UQ Excellence in Research Higher Degree Supervision award for encouraging student development through international student exchanges with overseas collaborators, whilst engendering internal cooperation within the study body.
Publications
Book Chapters
Laux, Christophe O., MacDonald, Megan E., Jacobs, Carolyn, Mariotto, Pierre, Tibere-Inglesse, Augustin, McGuire, Sean D., Zander, Fabian, Morgan, Richard, Savino, Luigi, De Cesare, Mario, Ceglia, Giuseppe, Del Vecchio, Antonio, Paganucci, Fabrizio and D'Orazio, Massimo (2019). Experimental investigation of meteorites: ground test facilities. Hypersonic meteoroid entry physics. (pp. 11-1-11-41) edited by Gianpiero Colonna, Mario Capitelli and Annarita Laricchiuta. Bristol, United Kingdom: IOP Publishing. doi: 10.1088/2053-2563/aae894ch11
Gildfind, David, Morgan, Richard G. and Jacobs, Peter A. (2016). Expansion tubes in Australia. Experimental methods of shock wave research. (pp. 399-431) edited by Ozer Igra and Friech Seiler. Basel, Switzerland: Springer. doi: 10.1007/978-3-319-23745-9_13
Jacobs, C. M., Morgan, R. G., Eichmann, T. N. and McIntyre, T. J. (2012). Radiative heat transfer measurements in a nonreflected shock tube at low pressures. 28th International Symposium on Shock Waves. (pp. 1069-1074) Berlin, Heidelberg: Springer Berlin Heidelberg. doi: 10.1007/978-3-642-25685-1_162
Morgan, R. G. (2001). Free Piston-Driven Reflected Shock Tunnels. Handbook of Shock Waves. (pp. 587-601) edited by Gabi Ben-Dor, Ozer Igra and Tov Elperin. USA: Academic Press.
Morgan, 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.
Journal Articles
Martinez Schramm, J., Dillmann, A., Hornung, H., Ito, K., Grabe, M., Karl, S., Klar, P., Morgan, R., Paull, A. and Steelant, J. (2022). In memoriam Prof. Klaus Hannemann (1959–2021). Shock Waves, 32 (4), 391-393. doi: 10.1007/s00193-022-01074-6
Liu, Yu, James, Christopher M., Morgan, Richard G., Jacobs, Peter A., Gollan, Rowan and McIntyre, Timothy J. (2022). Electron number density measurements in a Saturn entry condition. AIAA Journal, 60 (3), 1303-1315. doi: 10.2514/1.j060560
Gu, Sangdi, Morgan, Richard G., McIntyre, Timothy J. and Brandis, Aaron M. (2022). An experimental study of CO2 thermochemical nonequilibrium. AIAA Journal, 60 (3), 1283-1292. doi: 10.2514/1.J061037
Ramesh, Ranjini, Morgan, Richard G. and Mee, David J. (2022). Heat transfer measurements in an expansion tube using infrared thermography. AIAA Journal, 60 (2), 883-891. doi: 10.2514/1.J059919
Collen, Peter, Doherty, Luke J., Subiah, Suria D., Sopek, Tamara, Jahn, Ingo, Gildfind, David, Penty Geraets, Rowland, Gollan, Rowan, Hambidge, Christopher, Morgan, Richard and McGilvray, Matthew (2021). Development and commissioning of the T6 Stalker Tunnel. Experiments in Fluids, 62 (11) 225. doi: 10.1007/s00348-021-03298-1
Whitside, R. W., Chan, W. Y. K., Smart, M. K. and Morgan, R. G. (2021). The effect of increased throat size on the nozzle-supply flow in reflected shock tunnels. Shock Waves, 31 (5), 419-426. doi: 10.1007/s00193-021-01017-7
Fahy, Elise J., Buttsworth, David R., Gollan, Rowan J., Jacobs, Peter A., Morgan, Richard G. and James, Christopher M. (2021). Experimental and computational fluid dynamics study of Hayabusa reentry peak heating. Journal of Spacecraft and Rockets, 58 (6), 1-14. doi: 10.2514/1.a34863
Ravichandran, Ranjith, Lewis, Steven W., James, Christopher M., Morgan, Richard G. and McIntyre, Timothy J. (2020). Graphite ablation and radiation on interaction with hypervelocity earth-entry flows. Journal of Thermophysics and Heat Transfer, 35 (2), 1-14. doi: 10.2514/1.t5928
James, Christopher M., Lewis, Steven W., Morgan, Richard G., Liu, Yu and Lefevre, Alexis (2020). Generating High-Speed Earth Reentry Test Conditions in an Expansion Tube. Journal of Spacecraft and Rockets, 58 (2), 1-18. doi: 10.2514/1.a34821
Liu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy J. (2020). Experimental validation of a test gas substitution for simulating non-equilibrium giant planet entry conditions in impulse facilities. Experiments in Fluids, 61 (9) 198. doi: 10.1007/s00348-020-03032-3
Sopek, Tamara, Brieschenk, Stefan, Vanyai, Tristan, Morgan, Richard G. and McIntyre, Timothy J. (2020). Single-shot temperature measurements in a scramjet combustor using thermally assisted laser-induced fluorescence. AIAA Journal, 58 (8), 3486-3498. doi: 10.2514/1.j058985
James, C. M., Smith, D. R., McLean, C., Morgan, R. G., Lewis, S. W., Toniato, P., Wei, H. and McIntyre, T. J. (2020). Using optically filtered high-speed imaging to characterise expansion tube operating conditions. Shock Waves, 30 (5), 523-544. doi: 10.1007/s00193-020-00948-x
James, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W. and McIntyre, Timothy J. (2020). Experimentally Simulating Giant Planet Entry in an Expansion Tube. Journal of Spacecraft and Rockets, 57 (4), 1-16. doi: 10.2514/1.a34457
Sopek, Tamara, Brieschenk, Stefan, Vanyai, Tristan, Morgan, Richard G. and McIntyre, Timothy J. (2020). Iron contamination in high-enthalpy test facilities: OH PLIF imaging considerations. Journal of Propulsion and Power, 36 (1), 129-137. doi: 10.2514/1.B37676
Sheikh, Umar A., Wei, Han, Lewis, Steven W., James, Christopher M., Leyland, Pénélope, Morgan, Richard G. and McIntyre, Timothy J. (2020). Correction: Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in x2 (AIAA Journal, (2017), 55, 12, (4167-4180), 10.2514/1.J056021). AIAA Journal, 58 (11), AU2-AU2. doi: 10.2514/1.J056021.c1
Toniato, P., Gildfind, D. E., Jacobs, P. A. and Morgan, R. G. (2019). Expansion tube nozzle design using a parallel simplex algorithm. Shock Waves, 30 (2), 185-199. doi: 10.1007/s00193-019-00930-2
Ravichandran, Ranjith, Buttsworth, David R., Lewis, Steven W., Morgan, Richard G. and McIntyre, Timothy J. (2019). Filtered image thermography for high temperatures in hypersonic preheated ablation experiments. Journal of Thermophysics and Heat Transfer, 33 (4), 1074-1084. doi: 10.2514/1.T5629
James, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W. and McIntyre, Timothy J. (2019). Simulating gas giant atmospheric entry using helium and neon test gas substitutions. Journal of Spacecraft and Rockets, 56 (3), 725-743. doi: 10.2514/1.a34282
Apirana, Steven F. T., James, Christopher M., Eldridge, Robert, Morgan, Richard G. and Lewis, Steven W. (2019). Rapid prototyping for hypervelocity impulse facility test models. Aerospace Science and Technology, 88, 174-184. doi: 10.1016/j.ast.2019.03.024
James, Christopher M., Cullen, Timothy G. , Wei, Han, Lewis, Steven W., Gu, Sangdi, Morgan, Richard G. and McIntyre, Timothy J. (2018). Improved test time evaluation in an expansion tube. Experiments in Fluids, 59 (5) 87. doi: 10.1007/s00348-018-2540-1
James, C. M., Gildfind, D. E., Lewis, S. W., Morgan, R. G. and Zander, F. (2018). Implementation of a state-to-state analytical framework for the calculation of expansion tube flow properties. Shock Waves, 28 (2), 349-377. doi: 10.1007/s00193-017-0763-3
de Crombrugghe, G., Chazot, O., McIntyre, T. J. and Morgan, R. (2017). Experimental evidence of the impact of radiation coupling on binary scaling applied to shock layer flows. International Journal of Heat and Mass Transfer, 120, 568-574. doi: 10.1016/j.ijheatmasstransfer.2017.12.071
Gildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. K. and Gollan, R. J. (2017). Scramjet test flow reconstruction for a large-scale expansion tube, part 1: quasi-one-dimensional modelling. Shock Waves, 28 (4), 1-21. doi: 10.1007/s00193-017-0785-x
Gildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. C. and Gollan, R. J. (2017). Scramjet test flow reconstruction for a large-scale expansion tube, Part 2: axisymmetric CFD analysis. Shock Waves, 28 (4), 1-20. doi: 10.1007/s00193-017-0786-9
Lewis, Steven W., James, Christopher M., Ravichandran, Ranjith, Morgan, Richard G. and McIntyre, Timothy J. (2017). Carbon ablation in hypervelocity air and nitrogen shock layers. Journal of Thermophysics and Heat Transfer, 32 (2), 449-468. doi: 10.2514/1.T5270
Banerji, Nikhil, Leyland, Pénélope, Fahy, Elise and Morgan, Richard (2017). Earth reentry flow over a phenolic aeroshell in the X2 expansion tube. Journal of Thermophysics and Heat Transfer, 32 (2), 414-428. doi: 10.2514/1.T5255
Sheikh, Umar A., Wei, Han, Lewis, Steven W., James, Christopher M., Leyland, Pénélope, Morgan, Richard G. and McIntyre, Timothy J. (2017). Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in X2. AIAA Journal, 55 (12), 1-14. doi: 10.2514/1.J056021
Banerji, Nikhil, Leyland, Pénélope, Fahy, Elise and Morgan, Richard G. (2017). Venus entry flow over a decomposing aeroshell in X2 expansion tube. Journal of Thermophysics and Heat Transfer, 32 (2), 1-11. doi: 10.2514/1.T5172
Hermann, Tobias, Lohle, Stefan, Bauder, Uwe, Morgan, Richard, Wei, Han and Fasoulas, Stefanos (2017). Quantitative emission spectroscopy for superorbital reentry in expansion tube X2. Journal of Thermophysics and Heat Transfer, 31 (2), 257-268. doi: 10.2514/1.T4898
Lewis, Steven W., James, Christopher M., Morgan, Richard G., McIntyre, Timothy J., Alba, Christopher R. and Greendyke, Robert B. (2017). Carbon ablative shock layer radiation with high surface temperatures. Journal of Thermophysics and Heat Transfer, 31 (1), 193-204. doi: 10.2514/1.T4902
Sheikh, Umar A., Morgan, Richard G. and McIntyre, Timothy J. (2016). Optical thickness measurements of vacuum ultraviolet radiation in the X2 expansion tube. AIAA Journal, 54 (8), 2407-2417. doi: 10.2514/1.J054659
de Crombrugghe, G., Morgan, R. and Chazot, O. (2016). Theoretical approach and experimental verification of the role of diffusive transport under binary scaling conditions. International Journal of Heat and Mass Transfer, 97, 675-682. doi: 10.1016/j.ijheatmasstransfer.2016.02.018
Stalker, Caroline, Morgan, Richard and Tanner, Roger I. (2016). Raymond John Stalker 1930-2014. Historical Records of Australian Science, 27 (1), 70-80. doi: 10.1071/HR15012
Lewis, Steven W., Morgan, Richard G., McIntyre, Timothy J., Alba, Christopher R. and Greendyke, Robert B. (2016). Expansion tunnel experiments of earth reentry flow with surface ablation. Journal of Spacecraft and Rockets, 53 (5), 887-899. doi: 10.2514/1.A33267
Alba, Christopher R., Greendyke, Robert B., Lewis, Steven W., Morgan, Richard G. and McIntyre, Timothy J. (2016). Numerical modeling of Earth reentry flow with surface ablation. Journal of Spacecraft and Rockets, 53 (1), 84-97. doi: 10.2514/1.A33266
Gildfind, D.E. and Morgan, Richard G. (2015). A new sliding joint to accommodate recoil of a free-piston-driven expansion tube facility. Shock Waves Journal, 26 (6), 825-833. doi: 10.1007/s00193-015-0609-9
Sheikh, Umar A., Morgan, Richard G. and McIntyre, Timothy J. (2015). Vacuum ultraviolet spectral measurements for superorbital earth entry in X2 expansion tube. AIAA Journal, 53 (12), 3589-3602. doi: 10.2514/1.J054027
Gildfind, David E., James, Chris M., Toniato, Pierpaolo and Morgan, Richard G. (2015). Performance considerations for expansion tube operation with a shock-heated secondary driver. Journal of Fluid Mechanics, 777, 364-407. doi: 10.1017/jfm.2015.349
Gildfind, D. E., James, C. M. and Morgan, R. G. (2015). Free-piston driver performance characterisation using experimental shock speeds through helium. Shock Waves, 25 (2), 169-176. doi: 10.1007/s00193-015-0553-8
MacDonald, Megan E., Jacobs, Carolyn M., Laux, Christophe O., Zander, Fabian and Morgan, Richard G. (2015). Measurements of Air Plasma/Ablator Interactions in an Inductively Coupled Plasma Torch. Journal of Thermophysics and Heat Transfer, 29 (1), 12-23. doi: 10.2514/1.T4402
Zander, F., Gollan, R. J., Jacobs, P. A. and Morgan, R. G. (2014). Hypervelocity shock standoff on spheres in air. Shock Waves, 24 (2), 171-178. doi: 10.1007/s00193-013-0488-x
Gildfind, David E. and Morgan, Richard G. (2014). A new shock tube configuration for studying dust-lifting during the initiation of a coal dust explosion. Journal of Loss Prevention in the Process Industries, 29 (1), 198-208. doi: 10.1016/j.jlp.2014.02.011
Gildfind, David, Morgan, Richard G., Jacobs, Peter A. and McGilvray, Matthew (2014). Production of high-Mach-number scramjet flow conditions in an expansion tube. AIAA Journal, 52 (1), 162-177. doi: 10.2514/1.J052383
Capra, Bianca R. and Morgan, Richard G. (2013). Total heat transfer measurements on a flight investigation of reentry environment model. Journal of Spacecraft and Rockets, 50 (3), 494-503. doi: 10.2514/1.A32333
Zander, Fabian, Smart, Michael K., Drennan, John, Morgan, Richard G. and Wheatley, Brad (2013). Extreme materials in hypersonics. Materials Australia, 46 (1), 41-45.
Gildfind, D. E., Jacobs, P. A. and Morgan, R. G. (2013). Vibration isolation in a free-piston driven expansion tube facility. Shock Waves, 23 (5), 431-438. doi: 10.1007/s00193-013-0433-z
Zander, F., Morgan, R. G., Sheikh, U., Buttsworth, D. R. and Teakle, P. R. (2013). Hot-Wall Reentry Testing in Hypersonic Impulse Facilities. AIAA Journal, 51 (2), 476-484. doi: 10.2514/1.J051867
Buttsworth, David, Morgan, Richard and Jenniskens, Peter (2013). Near-Ultraviolet Emission Spectroscopy of the Hayabusa Reentry. Journal of Spacecraft and Rockets, 50 (6), 1109-1120. doi: 10.2514/1.A32500
Capra, Bianca and Morgan, Richard G. (2012). Radiative and total heat transfer measurements to a Titan Explorer model. Journal of Spacecraft and Rockets, 49 (1), 12-23. doi: 10.2514/1.52961
Gildfind, D. E., Morgan, R. G., McGilvray, M., Jacobs, P. A., Stalker, R. J. and Eichmann, T. N. (2011). Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions. Shock Waves, 21 (6), 559-572. doi: 10.1007/s00193-011-0336-9
Brandis, Aaron M., Morgan, Richard G. and McIntyre, Timothy J. (2011). Analysis of nonequilibrium CN radiation encountered during titan atmospheric entry. Journal of Thermophysics and Heat Transfer, 25 (4), 493-499. doi: 10.2514/1.50966
Dann, Andrew G. and Morgan, Richard G. (2011). Analytical method of prediction of turbulent boundary-layer separation in hypersonic flows. AIAA Journal, 49 (9), 2068-2072. doi: 10.2514/1.J050673
McGilvray, Matthew, Morgan, Richard G. and Jacobs, Peter A. (2010). Scramjet experiments in an expansion tunnel: Evaluated using a quasi- steady analysis technique. AIAA Journal, 48 (8), 1635-1646. doi: 10.2514/1.J050024
D'Souza, Mary G., Eichmann, Troy N., Potter, Daniel F., Morgan, Richard G., McIntyre, Timothy J., Jacobs, Peter A. and Mudford, Neil R. (2010). Observation of an ablating surface in expansion tunnel flow. AIAA Journal, 48 (7), 1557-1560. doi: 10.2514/1.J050207
Brandis, Aaron M., Morgan, Richard G., McIntyre, Tim and Jacobs, Peter A. (2010). Nonequilibrium radiation intensity measurements in simulated Titan atmospheres. Journal of Thermophysics and Heat Transfer, 24 (2), 291-300. doi: 10.2514/1.44482
McGilvray, M., Jacobs, P.A., Morgan, R.G., Gollan, R.J. and Jacobs, C.M. (2009). Helmholtz Resonance of Pitot Pressure Measurements in Impulsive Hypersonic Test Facilities. AIAA Journal, 47 (10), 2430-2439. doi: 10.2514/1.42543
McGilvray, M., Austin, J. M., Sharma, M., Jacobs, P. A. and Morgan, R. G. (2009). Diagnostic modelling of an expansion tube operating condition. Shock Waves, 19 (1), 59-66. doi: 10.1007/s00193-009-0187-9
McGilvray, M and Morgan, RG (2009). Effects of Upstream Injection on Scramjet Performance Using an Entropy-Based Method. JOURNAL OF PROPULSION AND POWER, 25 (2), 295-302. doi: 10.2514/1.38325
Silvester, T. B. and Morgan, R. G. (2008). Skin-friction measurements and flow establishment within a long duct at superorbital speeds. AIAA Journal, 46 (2), 527-536. doi: 10.2514/1.32668
Abdel-Jawad, Madhat M., Mee, David J. and Morgan, Richard G. (2007). New calibration technique for multiple-component stress wave force balances. Review of Scientific Instruments, 78 (6) 065101, 065101-1-065101-7. doi: 10.1063/1.2744235
Silvester, T.B., McIntyre, T.J. and Morgan, R.G. (2007). Superorbital expansion tube tests of a caret waverider. Shock Waves, 17 (1-2), 51-63. doi: 10.1007/s00193-007-0100-3
Stalker, R. J., Paull, A., Mee, D. J., Morgan, R. G. and Jacobs, P. A. (2005). Scramjets and Shock Tunnels: The Queensland Experience. Progress in Aerospace Sciences, 41 (6), 471-513. doi: 10.1016/j.paerosci.2005.08.002
McIntyre, T. J., Lourel, I., Eichmann, T. N., Morgan, R. G., Jacobs, P. A. and Bishop, A. I. (2004). Experimental expansion tube study of the flow over a toroidal ballute. Journal of Spacecraft And Rockets, 41 (5), 716-725. doi: 10.2514/1.13104
Wheatley, Vincent, Chiu, Sam Hsieh-Hsiang, Jacobs, Peter A., Macrossan, Michael N., Mee, David J. and Morgan, Richard G. (2004). Rarefied, Superorbital Flows in an Expansion Tube. International Journal for Numerical Methods for Heat and Fluid Flow, 14 (4), 512-537. doi: 10.1108/09615530410532277
Stalker, 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
Hayne, 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
Inger, 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
Stewart, 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
Shi, 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.
Inger, 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
Sutcliffe, 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
Wegener, 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
Sasoh, 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
Doolan, C. J. and Morgan, R. G. (1999). A two-stage free piston driver. Shock Waves, 9 (4), 239-248. doi: 10.1007/s001930050161
Shmelev, 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.
Kendall, 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
Buttsworth, 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
Wegener, 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
Buttsworth, 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
Buttsworth, 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
Neely, AJ and Morgan, RG (1994). The Superorbital Expansion Tube Concept, Experiment and Analysis. Aeronautical Journal, 98 (973), 97-105. doi: 10.1017/S0001924000050107
He, 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
Bakos Robert J. and Morgan Richard G. (1994). Chemical recombination in an expansion tube. AIAA journal, 32 (6), 1316-1319. doi: 10.2514/3.12135
Brescianini, 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
Stalker, 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
Morgan, 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.
Morgan, 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
MORGAN, R (1986). CONDUCT UNBECOMING - THE SOCIAL CONSTRUCTION OF POLICE DEVIANCE AND CONTROL - PUNCH,M. Journal of Management Studies, 23 (4), 470-473. doi: 10.2514/3.25831
Stalker, RJ and Morgan, RG (1984). Supersonic Hydrogen Combustion with a Short Thrust Nozzle. Combustion and Flame, 57 (1), 55-70. doi: 10.1016/0010-2180(84)90137-8
Morgan, RG and Stalker, RJ (1983). Fast Acting Hydrogen Valve. Journal of Physics E-Scientific Instruments, 16 (3) 009, 205-207. doi: 10.1088/0022-3735/16/3/009
Stalker, RJ and Morgan, RG (1982). Parallel Hydrogen Injection Into Constant-Area, High-Enthalpy, Supersonic Air-Flow. Aiaa Journal, 20 (10), 1468-1469. doi: 10.2514/3.7987
Morgan, RG (1982). Solar Assisted Heat-Pump. Solar Energy, 28 (2), 129-135. doi: 10.1016/0038-092X(82)90291-2
Conference Papers
Singh, M., Liu, Y., James, C.M., Morgan, R.G., Temme, N. and McIntyre, T.J. (2023). Preliminary results for CO2 recombination for low velocity, high density mars aerocapture conditions. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023.
Lock, S., Liu, Y., Morgan, R., James, C. and McIntyre, T. (2023). Experimental VUV shock layer radiation measurements for 13 and 14 km/s high speed earth re-entry conditions. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023.
Kennedy, Aaron, Penty Geraets, Rowland T., James, Christopher M., Thompson, Matthew, Morgan, Richard G., Austin, Joanna M., Zander, Fabian and McGilvray, Matthew (2023). Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in X3 Expansion Tunnel. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0271
Apirana, Steve F., James, Christopher M., Lewis, Steven and Morgan, Richard G. (2021). Experimental methods for studying post shock relaxation. AIAA Scitech 2021 Forum, Virtual, 11–15 and 19–21 January 2021. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-0446
Cullen, Timothy G., James, Christopher M., Ravichandran, Ranjith, Thompson, Matthew, Moran, Michael, Ramesh, Ranjini, Morgan, Richard G. and Nadesan, Thirukumaran (2021). Infrared thermography on a biconic model in Hypersonic expansion tube flows. AIAA Scitech 2021 Forum, Virtual, 11–15 and 19–21 January 2021. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-0873
Liu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy (2021). Self-absorption and electron number density measurements on Saturn entry radiation. AIAA Scitech 2021 Forum, Virtual, 11–15 and 19–21 January 2021. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-0209
Ramesh, Ranjini, Morgan, Richard G. and Mee, David J. (2021). A generalised calibration procedure for performing infrared thermography in expansion tubes. AIAA Aviation Forum, Virtual, 2-6 August 2021. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-2981
Liu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy J. (2020). Using aerothermodynamic similarity to experimentally study nonequilibrium giant planet entry. Joint Thermophysics and Heat Transfer Conference, Atlanta, GA, United States, 25-29 June 2018. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.a34713
James, Christopher M., Liu, Yu and Morgan, Richard (2020). Simulating Uranus Entry in an Expansion Tube. AIAA AVIATION 2020 FORUM , Virtual Event, 15-19 June 2020. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-3110
Stennett, Samuel J., Gildfind, David, Jacobs, Peter, Morgan, Richard, James, Christopher and Toniato, Pierpaolo (2020). The X3R Free-Piston Reflected Shock Tunnel: Australia's New Large-Scale, Long-Duration Hypersonic Testing Capability. 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Montreal, Canada , March 10-12, 2020. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-2447
Ramesh, Ranjini, Morgan, Richard, Ravichandran, Ranjith and Mee, David (2020). Infrared thermography in expansion tubes for Martian entry flows. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Montréal, Québec, Canada, 10-12 March 2020. Reston, Virginia: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-2415
Geraets, Rowland T. Penty, McGilvray, Matthew, Doherty, Luke J., Morgan, Richard G., James, Christopher M. and Buttsworth, David R. (2020). Development of a fast-response diamond calorimeter heat transfer gauge. 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, CO USA, 5-9 June 2017. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.t5688
James, Christopher M., Ravichandran, Ranjith, Smith, Daniel R., Cullen, Timothy G. and Morgan, Richard (2020). Scaled Apollo Heating Testing in a Large Expansion Tube. AIAA AVIATION 2020 FORUM , Virtual Event, 15-19 June 2020. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-3278
James, Christopher M., Birch, Byrenn, Smith, Daniel R., Cullen, Timothy G., Millard, Theodore, Vella, Samuel, Liu, Yu, Morgan, Richard G., Stern, Nathan and Buttsworth, David (2019). Testing of ultra fast response, durable co-axial thermocouples for high enthalpy impulse facilities. AIAA Aviation 2019 Forum, Dallas, TX USA, 17-21 June 2019. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3007
Cullen, T., James, C., Gollan, R. and Morgan, R. (2019). Application of Infrared Thermography in an Expansion Tunnel. In: Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019). 32nd International Symposium on Shock Waves (ISSW32 2019), Singapore, (1139-1165). 14-19 July 2019. doi:10.3850/978-981-11-2730-4_0271-cd
James, Christopher M., Lewis, Steven W., Gildfind, David E., Morgan, Richard G., McIntyre, Timothy J. and Liu, Yu (2019). Generating High Speed Earth Re-entry Test Conditions in an Expansion Tube for Interplanetary Return Missions. 32nd International Symposium on Shock Waves (ISSW32 2019), Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0424-cd
Apirana, S.F.T., James, C.M., Lewis, S.W., Morgan, R.G. and Zander, F. (2019). Studying post-shock relaxation using a Mach Disk. 11th Asia-Pacific International Symposium on Aerospace Technology, Gold Coast, Australia, 4-6 December 2019. Gold Coast, Australia: Engineers Australia.
Andrianatos, Andreas, Gildfind, David and Morgan, Richard G. (2019). Driver condition development for high enthalpy operation of the X3 expansion tube. 31st International Symposium on Shock Waves, Nagoya, Japan, 9-14 July 2017. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-91017-8_37
Ramesh, Ranjini, Kelly, Rory, Cullen, Timothy G., Morgan, Richard G. and Mee, David J. (2019). Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared Thermography. AIAA Aviation 2019 Forum, Dallas, TX, United States, 17-21 June 2019. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3006
James, Christopher, Lewis, Steven, Gildfind, David, Morgan, Richard and McIntyre, Timothy (2019). Generating high speed earth re-entry test conditions in an expansion tube. 8th International Workshop on Radiation of High Temperature Gases, Madrid, Spain, 25-29 March 2019.
Liu, Yu, Toniato, Pierpaolo, James, Chris, Morgan, Richard and McIntyre, T.J. (2019). Multidimensional effects and self- absorption on spectroscopic observations of Saturn entry radiation. 11th Asia-Pacific International Symposium on Aerospace Technology, Gold Coast, Australia, 4-6 December 2019. Gold Coast, Australia: Engineers Australia.
Thompson, M., James, C.M. and Morgan, R.G. (2019). Development of a high enthalpy driver in an expansion tube for generating Uranus entry flow conditions. 11th Asia-Pacific International Symposium on Aerospace Technology, Gold Coast, Australia, 4-6 December 2019. Gold Coast, Australia: Engineers Australia.
Toniato, Pierpaolo, Gildfind, David, Jacobs, Peter A. and Morgan, Richard G. (2019). Optimisation and design of a fully instrumented Mach 12 nozzle for the X3 expansion tube. 31th International Symposium on Shock Waves, Nagoya, Japan, 9-14 July 2017. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-91017-8_108
Thompson, Matthew, James, Christopher M., Lewis, Steven W., Gildfind, David E. and Morgan, Richard G. (2019). Generating 5-km/s low density hypersonic test flows in an expansion tube for studying ultraviolet radiation. 32nd International Symposium on Shock Waves, Singapore, 14-19 July 2019. Singapore: ISSW. doi: 10.3850/978-981-11-2730-4_0337-cd
Stennett, S. J., Gildfind, D. E., Jacobs, P. A., Morgan, R. G., James, C. M. and Toniato, P. (2019). The X3R reflected shock tunnel: a new, long-duration operating mode for the X3 expansion tube. Asia Pacific International Symposium on Aerospace Technology (APISAT 2019), Gold Coast, QLD, Australia, 4-6 December 2019.
Ravichandran, R., Lewis, S.W., James, C.M., Morgan, R.G. and McIntyre, T.J. (2019). Expansion tube experiments of graphite ablation and radiation in hypervelocity earth-entry flows. 8th International Workshop on Radiation of High Temperature Gases, Madrid, Spain, 25-29 March 2019.
Collen, Peter L., Doherty, Luke, McGilvray, Matthew, Naved, Imran, Penty Geraets, Rowland T., Hermann, Tobias A., Morgan, Richard G. and Gildfind, David (2019). Commissioning of the T6 Stalker Tunnel. AIAA Scitech 2019 Forum, San Diego, CA, United States, 7-11 January 2019. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-1941
Cullen, T. G., James, C. M., Gollan, R. J. and Morgan, R. G. (2019). Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnel. 31st International Symposium on Shock Waves, Nagoya, Japan, 9-14 July 2017. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-91017-8_24
Liu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy (2019). Theoretical and experimental study of helium-neon substitution for Saturn entry radiation. AIAA Aviation 2019 Forum, Dallas, TX United States, 17-21 June 2019. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3134
Andrianatos, Andreas, Gildfind, David and Morgan, Richard (2019). Testing a full-scale Hayabusa Model in a large expansion tube. Asia Pacific International Symposium on Aerospace Technology (APISAT 2019), Gold Coast, QLD, Australia, 4-6 December 2019.
Gildfind, David, Smith, Daniel, Thompson, Owen, Jacobs, Peter, Morgan, Richard, Kelly, Rory and McIntyre, Tim (2019). Evaluation of electrically insulating coatings for magnetohydrodynamic aerobraking experimentation. 32nd International Symposium on Shock Waves (ISSW32), Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0014-cd
Temme, Nils, James, Christopher M., McIntyre, Timothy, Lewis, Steven W. and Morgan, Richard G. (2019). Hypervelocity boundary-layer flow with high-temperature surface ablation. AIAA Aviation 2019 Forum, Dallas, TX United States, 17-21 June 2019. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3135
Toniato, Pierpaolo, Gildfind, David E., Andrianatos, Andreas and Morgan, Richard G. (2018). Full free-stream mach 12 scramjet testing in expansion tubes. 36th AIAA Applied Aerodynamics Conference, 2018, Atlanta, GA United States, 25-29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-3818
James, Christopher M., Smith, Daniel R., McLean, Carl, Morgan, Richard G., Lewis, Steven W. and Toniato, Pierpaolo (2018). Improving high enthalpy expansion tube condition characterisation using high speed imagery. 34th AIAA Aerodynamic Measurement Technology and Ground Testing Conference 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2018-3805
Gildfind, David E., Jacobs, Peter A., Gollan, Rowan J., Toniato, Pierpaolo, McIntyre, Timothy J., Andrianatos, Andreas, James, Christopher M. and Morgan, Richard G. (2018). Flow characterization and modeling of the X2 and X3 expansion tubes. VKI Lecture Series STO-AVT-235 on Flow Characterization and Modeling of Hypersonic Wind Tunnels, Brussels, Belgium, 3-5 December 2018.
Donegan, Brian E., Greendyke, Robert B., Ravichandran, Ranjith, Lewis, Steven W., Morgan, Richard G., McIntyre, Timothy J. and Apostolov, Zlatomir D. (2018). Experimental analysis of the interaction of carbon and silicon ablation products with expanding hypersonic flows. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018, Orlando, FL, United States, 17-19 September 2018. Reston, VA, United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2018-5325
Eldridge, R., James, C.M., Apirana, S. and Morgan, R.G. (2018). Rapid prototyping in instrumented hypervelocity testing. 18th Australian Space Research Conference, Gold Coast, QLD, Australia, 24-26 September 2018.
Stennett, Samuel J., Gildfind, David E., Jacobs, Peter A. and Morgan, Richard G. (2018). Performance optimization of X3R: A new reflected shock tunnel mode for the X3 expansion tube. 34th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-3563
Liu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy J. (2018). Experimental study of saturn entry radiation with higher amount of diluent in an expansion tube. 12th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-4070
Wei, Han, Morgan, Richard G., McIntyre, Timothy J., Brandis, Aaron M. and Johnston, Christopher O. (2017). Experimental and numerical investigation of air radiation in superorbital expanding flow. 47th AIAA Thermophysics Conference, Denver, CO, United States, 5 - 9 June 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-4531
Gildfind, David and Morgan, Richard G. (2017). A new sliding joint to accommodate recoil of a free-piston driven expansion tube. The 30th International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-44866-4_105
James, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W. and McIntyre, Timothy J. (2017). Experimentally simulating gas giant entry in an expansion tube. 21st International Space Planes and Hypersonic Systems and Technologies Conference, Xiamen, China, 6 - 9 March 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-2152
Ravichandran, R., Lewis, S.W., James, C.M., Morgan, R.G. and McIntyre, T.J. (2017). Interaction of ablating carbon with expanding earth entry flows in the X2 expansion tube. 9th Ablation Workshop, Bozeman, MT, United States, 30-31 August 2017.
Geraets, Rowland T. Penty, McGilvray, Matthew, Doherty, Luke J., Morgan, Richard G., James, Christopher M., Vanyai, Tristan and Buttsworth, David R. (2017). Development of a fast-response calorimeter heat transfer gauge for hypersonic ground testing. 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, Colorado, 5-9 June 2017. American Institute of Aeronautics and Astronautics Inc, AIAA.
Wei, H., Morgan, R. G., Sheikh, U. A., Jacobs, P. A., Gollan, R. J. and McIntyre, T. J. (2017). Preliminary experimental investigation of air radiation in super-orbital expanding flow. International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-44866-4_8
Geraets, Rowland T. Penty, McGilvray, Matthew, Doherty, Luke J., Morgan, Richard G., James, Christopher M., Vanyai, Tristan and Buttsworth, David R. (2017). Development of a fast-response calorimeter gauge for hypersonic ground testing. AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, CO, United States, 5-9 June 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautic. doi: 10.2514/6.2017-3238
James, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W. and McIntyre, T. M. (2017). Simulating gas giant entry with increased helium diluent in an expansion tube. 30th International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. Cham, Switzerland: Springer International Publishing. doi: 10.1007/978-3-319-44866-4_104
Gu, Sangdi, Morgan, Richard G. and McIntyre, Timothy J. (2017). Study of afterbody radiation during mars entry in an expansion tube. 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, United States, 9 - 13 January 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-0212
Banerji, Nikhil, Leyland, Pénélope and Morgan, Richard G. (2016). Expansion tunnel ablation testing in venus entry condition. 46th AIAA Thermophysics Conference, Washington, DC, United States, 13 - 17 June 2016. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-3231
Toniato, P., Gildfind, D. E., Jacobs, P. A. and Morgan, R. G. (2016). Extension of the X3 expansion tube capabilities for Mach 12 scramjet testing: flow condition: development and nozzle optimization. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, Australia, 5-8 December 2-16. Perth, Australia: Australasian Fluid Mechanics Society.
Leyland, Pénélope, Sheikh, Umar, Duval, Basil, Hermann, Tobias, Loehle, Stefan, McIntyre, Timothy J., Morgan, Richard, Wei, Han, Bouilly, Jean-Marc and Marraffa, Lionel (2016). The ESA ARC project: Ablation radiation coupling for hypervelocity re-entry with low density type ablators. 46th AIAA Thermophysics Conference 2016, Washington, DC United States, 13-17 June 2016. Reston, VA United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2016-3234
Fahy, Elise J., Gollan, Rowan J., Buttsworth, David R., Jacobs, Peter A. and Morgan, Richard G. (2016). Experimental and computational fluid dynamics studies of superorbital earth re-entry. 46th AIAA Thermophysics Conference, Washington, DC, United States, 13 - 17 June 2016. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-3532
Mora-Monteros, Jérémy, Leyland, Pénélope, Hannema, Gwenael, Sheikh, Umar, Fahy, Elise, Morgan, Richard G. and Morgan, Timothy J. (2016). Analysis and rebuilding of experiments on a heated carbon graphite model in the X2 expansion tube. 46th AIAA Thermophysics Conference, Washington, DC, United States, 13 - 17 June 2016. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-4155
Toniato, Pierpaolo, Gildfind, David and Morgan, Richard G. (2016). Current progress of the development of a Mach 12 scramjet operating condition in the X3 expansion tube. 11th International Workshop on Shock Tube Technology, Gottingen, Germany, 30 June -2 July 2016.
Toniato, Pierpaolo, Gildfind, David E., Jacobs, Peter A. and Morgan, Richard G. (2016). Development of a new Mach 12 scramjet operating capability in the X3 expansion tube. Asia-Pacific International Symposium on Aerospace Technology (APISAT), Cairns, QLD, Australia, 25 – 27 November 2015.
Andrianatos, A., Gildfind, D. and Morgan, R. (2016). Preliminary development of high enthalpy conditions for the X3 expansion tube. 20th Australasian Fluid Mechanics Conference, 20AFMC, Perth, WA, Australia, 5-8 December 2016. Australasian Fluid Mechanics Society.
Gildfind, D. E., Morgan, R. G. and Sancho, J. (2015). Design and commissioning of a new lightweight piston for the X3 Expansion Tube. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_57
Gildfind, D. E., Sancho Ponce, J. and Morgan, R. G. (2015). High Mach Number Scramjet Test Flows in the X3 Expansion Tube. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_58
Porat, Hadas, Zander, Fabian, Morgan, Richard G. and McIntyre, Timothy J. (2015). Emission spectroscopy of a mach disk at Titan atmospheric entry conditions. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July, 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_94
Zander, F., Jacobs, P. A., Gollan, R. J. and Morgan, R. G. (2015). Shock standoff on hemi-spherical bodies in hypervelocity flows. International Symposium on Shock Waves (ISSW29), Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_85
James, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W., Fahy, E. J. and McIntyre, T.J. (2015). Limits of Simulating Gas Giant Entry at True Gas Composition and True Flight Velocities in an Expansion Tube. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2-6 March 2015.
James, C., Gildfind, D., Morgan, R, Lewis, S., Fahy, E. and McIntyre, T. (2015). Simulating gas giant entry in an expansion tube. 7th Asia-Pacific International Symposium on Aerospace Technology, Cairns, Australia, 25-27 November 2015.
Jacobs, C. M., McIntyre, T. J., Morgan, R. G., Brandis, A. M. and Laux, C. O. (2015). Radiative heat transfer measurements in low-density titan atmospheres. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24–28 September 2012. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.T4519
Porat, Hadas and Morgan, Richard (2015). Radiative heatflux measurements for Titan atmospheric entry condition in superorbital expansion tunnel. International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015.
Morgan, Richard (2015). Study of ablative systems in expansion tubes. Ablation Workshop, Tullahoma, TN, United States, 21-22 October 2015.
Morgan, Richard (2015). Hypersonics Research in Australia. Air Force Office of Scientific Research, Arlington, VA, United States, 25 March 2015.
Morgan, Richard (2015). Duplication of atmospheric entry in laboratories: what are radiatively coupled flows?. International Planetary Probe Workshop, Cologne, Germany, 15-19 June 2015.
Andrianatos, Andreas, Gildfind, David and Morgan, Richard (2015). A study of radiation scaling of high enthalpy flows in expansion tubes. Asia-Pacific International Symposium on Aerospace Technology, Cairns, QLD, Australia, 25-27 November 2015.
James, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W., Fahy, Elise J. and McIntyre, Timothy J. (2015). On the current limits of simulating gas giant entry flows in an expansion tube. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6 - 9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3501
McGilvray, Matthew, Doherty, Luke, Morgan, Richard G. and Gildfind, David E. (2015). T6: The Oxford University Stalker Tunnel. International Space Planes and Hypersonic Systems and Technologies Conferences, Glasgow, Scotland, 6-9 July 2015. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3545
Lewis, Steven W., Morgan, Richard G., McIntyre, Timothy J., Alba, Christopher R. and Greendyke, Robert B. (2015). Comparison of carbon ablative shock-layer radiation with high surface temperatures. 45th AIAA Thermophysics Conference, Dallas, TX, United States, 22-26 June, 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-2348
Morgan, R. G. and Gildfind, D. E. (2015). Shock tube simulation of low Mach number blast waves. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_11
James, C .M., Gildfind, D. E., Morgan, R. G. and McIntyre, T. J. (2015). Working towards simulating gas giant entry radiation in an expansion tube. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_89
McGilvray, Matthew , Doherty, Luke , Morgan, Richard G. and Gildfind, David (2015). T6: The Oxford University Stalker Tunnel. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2-6 March 2015.
Sheikh, U. A., Jacobs, C., Laux, C. O., Morgan, R. G. and McIntyre, T. J. (2015). Measurements of radiating flow fields in the vacuum ultraviolet. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_104
Morgan, R., Rees, B., Rutherford, J., Jefferey, M., Sollart, M., Morris, N., Basore, K., James, C., Wei, H., Gu, S., Lewis, S. and Landsberg, W. (2015). Advanced hypersonic vehicle component testing using pre-heated models and infrared scanning. 7th Asia-Pacific International Symposium on Aerospace Technology (APISAT), Cairns, QLD, Australia., 25-27 November, 2015.
Morgan, Richard (2015). Transitional and Turbulent Heating in Re-Entry flow, Presentation to the meeting of NATO STO AVT-240 RTG-082 working group on Hypersonic Transition. Hypersonic Transition, Tuscon, Arizona, 26-27 March 2015.
Fahy, Elise , Buttsworth, David and Morgan, Richard (2015). Scaled earth re-entry experiments in the X2 expansion tube. Asia-Pacific International Symposium on Aerospace Technology, Cairns, QLD, Australia, 25 -27 November 2015.
Morgan, Richard G. and Wheatley, Brad J. (2015). Intercontinental rocket plane transport network. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3538
Fahy, Elise , Morgan, Richard G., McIntyre, Timothy J. and Buttsworth, David R. (2014). Scaled Hayabusa Experiments in the X2 Expansion Tube. 6th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, St Andrews, Scotland, United Kingdom, 24-28 November 2014.
James, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W., Fahy, E. J. and McIntyre, T. J. (2014). On the limits of simulating gas giant entry at true gas composition and true flight velocities in an expansion tube. 6th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, St Andrews, United Kingdom, 24-28 November 2014.
Brandis, Aaron M., Laux, Christophe O., Magin, Thierry, McIntyre, Timothy J. and Morgan, Richard G. (2014). Comparison of Titan entry radiation shock-tube data with collisional-radiative models. 40th AIAA Thermophysics Conference, Seattle, WA United States, 23 - 26 June 2008. Reston, VA United States: American Institute of Aeronautics and Astronautics, Inc.. doi: 10.2514/1.T4231
Wei, H., Chan, W. Y. K, Jacobs, P. A. and Morgan, R. G. (2014). Computational optimisation and analysis of a truncated hypersonic nozzle for X3 expansion tunnel. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.
James, Christopher, Gildfind, David, Morgan, Richard and McIntyre, Tim (2014). The limits of simulating gas giant entry at true gas composition and true flight velocities in an expansion tube. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.
Porat, H., Allsop, B. V., Morgan, R. G., Srinath, S., Reddy, K. P. J. and McIntyre, T. J. (2014). Amplifier design for new CNT radiation gauges in expansion tunnels. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.
Morgan, Richard G. and David Gildfind (2014). X3 reflected shock tunnel for extended flow duration. The 2014 Asia-Pacific International Symposium on Aerospace Technology, Shanghai China, 24-26 September 2014. Amsterdam, The Netherlands: Elsevier.
Sheikh, Umar A., Lewis, Steve, Wei, Han, Ibrahim, Mohammed, Morgan, Richard G. and McIntyre, Timothy J. (2014). Filtered Two-Dimensional Imaging in the X2 Expansion Tube. 6th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, St Andrews, United Kingdom, 24-28 November 2014.
de Crombrugghe, G., Gildfind, D., Zander, F., McIntyre, T. and Morgan, R. (2014). Design of test flows to investigate binary scaling in high enthalpy CO2-N2 mixtures. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.
Gildfind, D. E., James, C. M. and Morgan, R. G. (2014). Performance considerations for expansion tube operation with a shock-heated secondary driver. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.
Sheikh, U. A., Morgan, R. G., McIntyre, T. J. and Laux, C. O. (2013). Re-entry radiative heating studies in vacuum ultraviolet. ATW13: 4th Aerospace Thematic Workshop, Aussois, France, 7-12 April, 2013.
MacDonald, Megan E., Jacobs, Carolyn M., Laux, Christophe O. and Morgan, Richard G. (2013). Measurements of air plasma/ablator interactions in a 50 kW inductively coupled plasma torch. 44th AIAA Thermophysics Conference, San Diego, United States, 24-27 June 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-2772
Porat, Hadas, Sheikh, Umar A., Morgan, Richard G., Eichmann, Troy N. and McIntyre, Timothy J. (2013). Vacuum ultraviolet and ultraviolet emission spectroscopy measurements for Titan and Mars atmospheric entry conditions. 44th AIAA Thermophysics Conference, San Diego, CA, USA, 24-27 June, 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-2647
James, Christopher M., Gildfind, David E., Morgan, Richard G. and McIntyre, Timothy J. (2013). Theoretical validation of a test gas substitution for expansion tube simulation of gas giant entry. 44th AIAA Thermophysics Conference, San Diego, United States, 24-27 June 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-2506
Sheikh, Umar A., Morgan, Richard G., McIntyre, Timothy J. and Laux, Christophe O. (2013). Through surface and across surface vacuum ultraviolet spectral measurements in an expansion tube. 44th AIAA Thermophysics Conference, San Diego, United States, 24-27 June 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-2644
Jacobs, C., MacDonald, M., Zander, F., Morgan, R. and Laux, C.O. (2013). Ablation/radiation studies in the Ecole Centrale plasma torch facility. ATW13: 4th Aerospace Thematic Workshop, Aussois, France, 7-12 April, 2013.
Jacobs, Carolyn, MacDonald, M. E., Zander, F., Morgan, R. G. and Laux, C. O. (2013). Radiation in low density hypervelocity flows: application to Titan entry. ARA 2013: 4th International ARA Days, Arcachon, France, 27-29 May, 2013.
James, Chris, Gildfind, David, Morgan, Richard G., Jacobs, Peter A. and Zander, Fabian (2013). Designing and simulating high enthalpy expansion tube conditions. APISAT 2013: 2013 Asia-Pacific International Symposium on Aerospace Technology, Takamatsu, Japan, 20-22 November 2013. Takamatsu, Japan: Japan Society for Aeronautical and Space Sciences.
Jacobs, C. M., Sheikh, U. A., MacDonald, M. E., Morgan R. G. and Laux, C. O. (2013). Vacuum ultraviolet radiation studies in a plasma torch facility. EUCASS 2013: 5th European Conference for Aeronautics and Space Sciences, Munich, Germany, 1-4 July, 2013.
Jacobs, Peter, Morgan, Richard, Brandis, Aaron, Buttsworth, David, Dann, Andrew, D'Souza, Mary, Eichmann, Troy, Gildfind, David, Gollan, Rowan, Jacobs, Carolyn, McGilvray, Matthew, McIntyre, Tim, Mudford, Neil, Porat, Hadas, Potter, Dan and Zander, Fabian (2013). Design, operation and testing in expansion tube facilities for super-orbital re-entry. STO-AVT-VKI Lecture Series Radiation and Gas-Surface Interaction Phenomena in High Speed Re-Entry (2013-AVT-218), Rhode-St-Genèse, Belgium, 6-8 May 2013.
MacDonald, M. E., Jacobs, C. M., Laux, C. O., Zander, F. and Morgan, R.G. (2013). Characterization of a 50 kW Inductively Coupled Plasma Torch for use in Testing of Ablative Materials. 7th European Workshop on Thermal Protection Systems and Hot Structures, Noordwijk, The Netherlands, 8 - 10 April 2013.
Jacobs, C. M., Sheikh, U. A., MacDonald, M. E., Laux, C. O. and Morgan, R. G. (2013). Vacuum ultraviolet radiation studies in a plasma torch facility from 170-200 nm. 44th AIAA Thermophysics Conference, San Diego, United States, 24-27 June 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-3015
Zander, Fabian, Morgan, Richard G., Molder, Sannu, Jacobs, Peter A., Gollan, Rowan, Porat, Hadas and McIntyre, Timothy J. (2012). Mach disk platform for studying radiating flows. 5th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Barcelona, Spain, 16-19 October 2012. Noordwijk, The Netherlands : ESA Communications .
Morgan, R. G., Sheikh, U. A. and Gildfind, D. E. (2012). Standing shock formation in a non-reflected shock tube. International Symposium on Shock Waves (28th, ISSW28), Manchester, U.K., 17-22 July 2011. Heidelberg, Germany: Springer. doi: 10.1007/978-3-642-25685-1_87
Fahy, E. J., Zander, F., Buttsworth, D. R. and Morgan, R. G. (2012). Fast-response pyrometer development for expansion tunnel testing with hot carbon models. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3-7 December 2012. Hawthorn, Vic., Australia: Australasian Fluid Mechanics Society.
James, C. M. and Morgan, R. M. (2012). Radiation from simulated atmospheric entry into the gas giants. 18th Australasian Fluid Mechanics Conference (AFMC), Launceston, Australia, 3-7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.
Buttswoth, David, Morgan, Richard and Jenniskens, Peter (2012). Near ultraviolet emission spectroscopy of the Hayabusa re-entry. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, United States, 9-12 January 2012. Reston, VA, U.S.A.: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-1297
Sheikh, Umar A., Morgan, Richard G., Zander, Fabian, Eichmann, Troy N. and McIntyre, Timothy J. (2012). Vacuum ultraviolet emission spectroscopy system for superorbital re-entries. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24-28 September 2012. Reston, VA, U.S.A.: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-5807
Zander, F., Molder, S., Morgan, R. G., Jacobs, P. A. and Gollan, R. J. (2012). High temperature gas effects for converging conical shocks. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, 24 - 28 September 2012. Red Hook, N.Y: Currans. doi: 10.2514/6.2012-5939
Jacobs, C. M., Morgan, R. G., McIntyre, T. J. and Laux, C. O. (2012). Radiative heat transfer measurements in low density titan atmospheres. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, 24 - 28 September 2012. Red Hook, N.Y: Currans. doi: 10.2514/6.2012-5921
Dann, A. G., Morgan, R. G., Gildfind, D. E., Jacobs, P. A., McGilvray, M. and Zander, F. (2012). Upgrade of the X3 super-orbital expansion tube. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3-7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.
Porat, Hadas, Morgan, Richard G. and McIntyre, Timothy J. (2012). Study of radiative heat transfer in titan atmospheric entry. 28th International Congress of the Aeronautical Sciences (ICAS 2012), Brisbane, Australia, 23-28 September 2012. United Kingdom: International Council of the Aeronautical Sciences (ICAS).
Porat, Hadas, Morgan, Richard G. and McIntyre, Timothy J. (2012). Study of radiative heat transfer in titan atmospheric entry. 18th Australasian Fluid Mechanics Conference, Launceston, TAS, Australia, 3-7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.
Zander, F., Jacobs, P. A., Sheikh, U. A., Buttsworth, D. R. and Morgan, R. G. (2012). High speed imaging of X2 expansion tube flows. 30th International Congress on High-Speed Imaging and Photonics, Pretoria, South Africa, 16-21 September 2012. Johannesburg, South Africa: University of the Witwatersrand, School of Mechanical, Industrial and Aeronautical Engineering.
Gildfind, D. E., Morgan, R. G. and Jacobs, P. A. (2012). Vibration isolation in a free-piston driven Expansion tube. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3-7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.
Gildfind, D. E., Morgan, R. G., McGilvray, M., Jacobs, P. A., Stalker, R. J. and Eichmann, T. N. (2012). Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions. International Symposium on Shock Waves (28th, ISSW, 2011), Manchester, U. K., 17-22 July 2011. Heidelberg, Germany: Springer. doi: 10.1007/978-3-642-25685-1_150
Leyland, Pénélope, McIntyre, Timothy J., Sheikh, Umar, Eichmann, Troy N., Morgan, Richard G., Loehle, Stefan, Hermann, Tobias, De Filippis, Federico, Trifoni, Eduardo and Cillo, Giovanni (2012). VUV radiation measurements for radiation ablation coupling. 5th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Barcelona, Spain, 16-19 October 2012. Noordwijk, The Netherlands : ESA Communications .
Jacobs, C. M., Morgan, R. G., Eichmann, T. N. and McIntyre, T. J. (2012). Radiative heat transfer measurements in a nonreflected shock tube at low pressures. International Symposium on Shock Waves (28th, ISSW28), Manchester, U.K., 17-22 July 2011. Heidelberg, Germany: Springer.
Gildfind, D. E., Morgan, R. G., McGilvray, M. and Jacobs, P. A. (2012). High mach number and total pressure flow conditions for scramjet testing. International Symposium on Shock Waves (28th, ISSW28), Manchester, U.K., 17-22 July 2011. Heidelberg, Germany: Springer. doi: 10.1007/978-3-642-25685-1_42
Gildfind, David E., Morgan, Richard G., McGilvray, Matthew and Jacobs, Peter (2012). Simulation of high mach number scramjet flow conditions using the X2 expansion tube. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24-28 September 2012. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-5954
Morgan, Richard G. and McIntyre, Timothy J. (2012). Study of hypervelocity non equilibrium flows in impulse facilities. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, United States, 9-12 January 2012. Reston, VA, U.S.A.: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-726
Zander, F., Jacobs, P. A., Sheikh, U. A. and Morgan, R. G. (2012). High speed imaging of spherical shock standoff in hypervelocity flows. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3-7 December 2012. Hawthorn, Vic., Australia: Australasian Fluid Mechanics Society.
Sancho, J., Gildfind, D. E., Jacobs, P. A. and Morgan, R. G. (2012). Toward the full CFD Simulation of expansion tubes. 18th Australasian Fluid Mechanics Conference, Launceston, Australia, 3-7 December 2012. Hawthorn, VIC, Australia: Australasian Fluid Mechanics Society.
Zander, F., Morgan, R.G., Sheikh, U.A., Buttsworth, D. R. and Teakle, P. R. (2012). Hot wall testing methodology for impulse facilities. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, 24 - 28 September 2012. Red Hook, N.Y: Currans. doi: 10.2514/6.2012-5953
Morgan, Richard G., McIntyre, Timothy J. and Sheikh, Umar (2011). Simulation of radiating flows in impulsive facilities. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, United States, 4-7 January 2011. Reston, Virigina: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2011-250
Gildfind, D. E., Morgan, R. G., McGilvray, M., Jacobs, P. A., Eichmann, T., Stalker, R. J. and Teakle, P. (2010). Design of lightweight pistons for the X2 and X3 expansion tube free-piston drivers. 17AFMC: 17th Australasian Fluid Mechanics Conference, Auckland, New Zealand, 5-9 December 2010. Auckland, New Zealand: The University of Auckland.
Brandis, A. M., Cruden, B. A., Prabhu, D., Bose, D., McGilvray, M. and Morgan, R. G. (2010). Analysis of air radiation measurements obtained in the EAST and X2 shocktube facilities. 10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, Chicago, IL, U.S.A., 28 June-1 July 2010. Reston, VA, U.S.A.: American Institute of Aeronautics & Astronautics (AIAA).
D'Souza, M. G., Eichmann, T. N., Potter, D. F., Mudford, N. R., Morgan, R. G. and McIntyre, T. J. (2010). An experimental investigation of radiation over an ablating stardust model at 9.8 KM/S. 61st International Astronautical Congress 2010, IAC 2010, Prague, 27 September - 1 October 2010. Paris, France: International Astronautical Federation.
Buttsworth, David R., D'Souza, Mary, Potter, Daniel, Eichmann, Troy N., Mudford, Neil, McGilvray, Matthew, McIntyre, Timothy J., Jacobs, Peter A. and Morgan, Richard G. (2010). Expansion tunnel radiation experiments to support hayabusa re-entry observations. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, USA, 4-7 January 2010. Reston, VA, United States: American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/6.2010-634
Morgan, R. G. (2010). Modeling of radiating flows in the atmospheres of the Gas Giants. 17th Australasian Fluid Mechanics Conference 2010, 17AFMC, Auckland, New Zealand, 5 - 9 December 2010. Auckland NZ: University of Auckland, Dept. of Mechanical Engineering.
D'Souza, M. G., Creagh, M. and Morgan, R. G. (2010). Design, construction and testing of sounding rocket payloads at the University of Queensland. 61st International Astronautical Congress 2010, IAC 2010, Prague, Czech Republic., 27 September 27 - 1 October 2010. Paris, France: International Astronautical Federation.
Rowan Gollan, Carolyn Jacobs, Jacobs, Peter A., Morgan, Richard G., McIntyre, Timothy J., Macrossan, Michael N., Buttsworth, David R., Eichmann, Troy N. and Daniel Potter (2009). A simulation technique for radiating shock tube flows. 26th International Symposium on Shock Waves (ISSW26), Gottingen, Germany, 15-20 July. Berlin, Germany: Springer-Verlag Heidelberg. doi: 10.1007/978-3-540-85168-4_74
Morgan, R. G. and Zander, F. (2009). Radiatively cooled scramjet combustor. 26th International Symposium on Shock Waves (ISSW26), Gottingen, Germany, 15-20 July 2007. Berlin, Germany: Springer. doi: 10.1007/978-3-540-85181-3_55
McIntyre, T. J., Eichmann, T. N., Mallon, M., Potter, D., Brandis, A., Jacobs, C., Morgan, R., Jacobs, P. and Buttsworth, D. (2009). The generation and measurement of high temperature radiating flows in a high enthalpy pulsed facility. 3rd International Workshop: Radiation of High Temperature Gases in Atmospheric Entry, Heraklion, Greece, 30 September - 3 October 2008. Noordwijk, The Netherlands: ESA Communication Production Office.
Dann, A. G. and Morgan, R. G. (2009). Experimental investigation of the effect of two incident shock waves on a turbulent boundary layer in hypersonic circular duct flows. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition [Papers], Orlando, FL United States, 5 - 8 January 2009. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2009-33
McGilvray, Matthew, Morgan, Richard G. and Jacobs, Peter A. (2009). Scramjet experiments in an expansion tunnel: Evaluated using a quasi- steady analysis technique. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, 19-22 October, 2009. Washington, DC, U.S.A.: AIAA - American Institute of Aeronautics and Astronautics. doi: 10.2514/1.J050024
Zander, Fabian and Morgan, Richard (2009). Composite scramjet combustor. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, 19 - 22 October 2009. Reston, VA United States: AIAA. doi: 10.2514/6.2009-7354
Brandis, A., McIntyre, T., Morgan, R. and Jacobs, P. (2009). Overview of radiation intensity measurements on the x2 facility at the university of queensland. 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Heraklion, Greece, 30 September – 3 October 2008. Noordwijk, The Netherlands: European Space Agency.
Brandis, Aaron, McIntyre, Tim, Morgan, Richard, Jacobs, Peter, Laux, Christophe and Magin, Thierry (2009). Nonequilibrium radiation modeling and experimentation relevant to titan entry. 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry , Heraklion, Greece, 30 September-3 October 2008. Noordwijik, The Netherlands: ESA Communication Production Office.
Jacobs, C. M. and Morgan, R. G. (2009). Radiation measurements in rarefied Titan atmospheres. 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, FL, 5 - 8 January 2009. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2009-1029
Silvester, T. B. and Morgan, R. G. (2008). Skin-friction measurements and flow establishment within a long duct at superorbital speeds. doi: 10.2514/1.32668
Potter, Daniel F., Gollan, Rowan J., Eichmann, Troy, McIntyre, Tim J., Morgan, Richard G. and Jacobs, Peter A. (2008). Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers. 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 7-10 january 2008.
Potter, Daniel F., Eichmann, Troy, Brandis, Aaron, Morgan, Richard G., Jacobs, Peter A. and McIntyre, Tim J. (2008). Simulation of radiating CO2–N2 shock layer experiments at hyperbolic entry conditions. 40th Thermophysics Conference, Seattle, Washington State, USA, 23-26 June 2008. Reston, Virigina: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2008-3933
Brandis, Aaron M., Morgan, Richard G., McIntyre, Tim and Jacobs, Peter A. (2008). Nonequilibrium radiation intensity measurements in simulated titan atmospheres. 26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Seattle, United States, 23-26 June 2008. Reston, VA, United States: American Institute of Aeronautics and Astronau. doi: 10.2514/6.2008-4136
Morgan, R. G., McIntyre, T. J., Buttsworth, D. R., Jacobs, P. A., Potter, D. F., Brandis, A. M., Gollan, R. J., Jacobs, C. M., Capra, B. R., McGilvray, M. and Eichmann, T. (2008). Impulse facilities for the simulation of hypersonic radiating flows. 38th Fluid Dynamics Conference and Exhibit, Seattle, Washington, U.S.A., 23 - 26 June, 2008. Reston, VA, U.S.A.: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2008-4270
McGilvray, M., Austin, J. M., Sharma, M, Jacobs, P. A. and Morgan, R. G. (2007). Diagnostic Modelling of an Expansion Tube Operating Condition for a Hypersonic Free Shear Layer Experiment. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 2-7 December 2007. Brisbane, Australia: School of Engineering, The University of Queensland.
Zander, F. and Morgan, R. G. (2007). Transient Heat Analysis of a Carbon Composite Scramjet Combustion Chamber. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Australia: School of Engineering, The University of Queensland.
Dann, A. G. and Morgan, R. G. (2007). CFD designed experiments for shock wave/boundary layer interactions in hypersonic ducted flows. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Australia: School of Engineering, The University of Queensland.
Brandis, A. M., Morgan, R. G., Laux, C. O., Magin, T., McIntyre, T. and Jacobs, P. A. (2007). Nonequilibrium radiation measurements and modelling relevant to Titan entry. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 2-7 December, 2007. Brisbane, Australia: School of Engineering, The University of Queensland.
Potter, D. F., Gollan, R. J., Eichmann, T., Jacobs, P. A., Morgan, R. G. and McIntyre, T. J. (2007). Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Queensland: School of Engineering, The University of Queensland.
Eichmann, T., Potter, D., McIntyre, T. J., Brandis, A., Mallon, M., Morgan, R. G. and Rubinsztein-Dunlop, H. (2007). Radiation measurements in a simulated non-terrestrial atmosphere. 16th Australasian Fluid Mechanics Conferences, Gold Coast, Australia, 2-7 December 2007. Brisbane: The University of Queensland.
Dann, A., Morgan, R. G. and McGilvray, M. (2007). Experimental study of two-dimensional shock wave/turbulent boundary layer interactions. 26th International Symposium on Shock Waves (ISSW26), Gottingen, Germany, 15-20 July 2007. Berlin & Heidelberg: Springer. doi: 10.1007/978-3-540-85181-3_74
Morgan, Richard, Paull, Allan, Smart, Michael and Stalker, Ray (2007). Hypersonics Research in Australia. AVT-150 RTO AVT/VKI Lecture Series: Advances on Propulsion Technology for High-Speed Aircraft, Von Karmen Institute for Fluid Mechanics, Rhode St. Genese, Belgium, 12-15 March 2007. Neuilly-sur-Seine, France: NATO Research and Technology Organisation.
McGilvray, Matthew, Jacobs, Peter A., Morgan, Richard G. and Ramanah, Dwishen (2007). Boundary Layer Transition in an Expansion Tube at a Low Enthalpy Operating Condition. 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 8 -11 January, 2007. Reston, VA: American Institute of Aeronautics and Astronautics, Inc.. doi: 10.2514/6.2007-1328
McGilvray, Matthew, Jacobs, Peter A. and Morgan, Richard G. (2006). Simulations of scramjet starting and establishment time in an expansion tunnel. 14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, , , November 6, 2006-November 9, 2006. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2006-8143
Capra, Bianca R. and Morgan, Richard G. (2006). Radiative and total heat transfer measurements to a Titan explorer model. AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference, Canberra, ACT, Australia, 6-9 November 2006. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2006-7934
McGilvray, M, Jacobs, P A and Morgan, R G (2006). Simulations of scramjet starting and establishment time in an expansion tunnel. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, 6-9 November 2006. USA: American Institute of Aeronautics and Astronautics.
Dann, A. G., Denman, A. W., Jacobs, P A and Morgan, R G (2006). Study of separating compressible turbulent boundary-layers. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, 6-9 November 2006. USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2006-7943
Morgan, Richard, McIntyre, Tim, Gollan, Rowan, Jacobs, Peter, Brandis, Aaron, McGilvray, Matthew, van Diem, Dwight, Gnoffo, Peter, Pulsonnetti, Maria and Wright, Michael (2006). Radiation measurements in nonreflected shock tunnels. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, California, USA, 5-8 June 2006. Reston, VA, U.S.A.: American Institute of Aeronautics and Astronautics.
Capra, B. R. and Morgan, R G (2006). Radiative and total heat transfer measurements to a Titan Explorer Model. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, ACT, Australia, 6-9 November 2006. U.S.A.: American Institute of Aeronautics and Astronautics.
Brandis, A. M., Gollan, R. J., Scott, M. P., Morgan, R. G. and Jacobs, P. A. (2006). Expansion tube operating conditions for studying nonequilibrium radiation relevant to Titan Aerocapture. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, California, USA, 9-12 July 2006. USA: American Institute of Aeronautics and Astronautics.
Morgan, Richard, Mcintyre, Tim, Gollan, Rowan, Jacobs, Peter, Brandis, Aaron, McGilvray, Matthew, Van Diem, Dwight, Gnoffo, Peter, Pulsonnetti, Maria V. and Wright, Michael (2006). Radiation measurements in nonreflected shock tunnels. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, CA, United States, 5-8 June 8 2006. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2006-2958
Brandis, A. M., Buttsworth, D. R., Capra, B. R., Eichmann, T., Gollan, R. J., Jacobs, C. M., Jacobs, P. A., Macrossan, M. N., McGilvray, M., McIntyre, T. J., Morgan, R. G., Potter, D. F., Scott, M. P. and van Diem, D. (2006). Impulse facility simulation of hypervelocity radiating flows. 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Rome, Italy, 6-8 September 2006. The Netherlands: ESA Publications.
McGilvray, Matthew, Teakle, Phillip, Jacobs, Peter and Morgan, Richard (2005). Geometrical Nozzle Design for Wagtail Rocket Motors. 5th Australian Space Science Conference, Melbourne (Hosted by RMIT), September 14 - 16, 2005.
Capra, BR, Morgan, RG and Leyland, P (2005). New gauge design to measure radiative heat transfer to a Titan aerocapture vehicle in expansion tubes. 5th European Symposium on Aerothermodynamics for Space Vehicles, Cologne, Germany, 8-11 November 2004. The Netherlands: ESA Publications.
Hayne, M. J., Gai, S. L., Mee, D. J. and Morgan, R. G. (2005). Real gas effects on flows over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. doi: 10.1007/978-3-540-27009-6_36
Jacobs, P. A., Silvester, T. B., Morgan, R. G., Scott ,M .P., Gollan, R. J. and McIntyre, T. J. (2005). Superorbital expansion tube operation: estimates of flow conditions via numerical simulation. 43rd AIAA Aerospace Science Meeting and Exhibit, Reno, Nevada, United States, 10 - 13 January 2005. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2005-694
McGilvray, M., Morgan, R. G., Paull, A., Abdel-Jawad, M. M., Jacobs, P. A., McIntyre, T. J. and Scott, M. A. (2005). Operating conditions in UQ's impulse facilities for scramjet testing. 25th International Symposium on Shock Waves, Bangalore, India, 17-22 July 2005.
Morgan, Richard G. (2005). Expansion tube investigations of planetary aerodynamics. 25th International Symposium on Shock Waves – ISSW25, Bangalore, India, 17-22 July 2005. Hyderabad, A.P., India: Universities Press (India).
Scott, Michael P., Morgan, Richard G. and Jacobs, Peter A. (2005). A new single stage driver for the X2 expansion tube. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers, Reno, NV USA, 10-13 January 2005. doi: 10.2514/6.2005-697
Hayne, MJ, Mee, DJ, Gai, SL, Stewart, BS and Morgan, RG (2005). Flow establishment over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing Peoples R China, Jul 11-16, 2004. BERLIN: SPRINGER-VERLAG BERLIN. doi: 10.1007/978-3-540-27009-6_23
Scott, MP, Jacobs, PA and Morgan, RG (2005). Nozzle development for an expansion tunnel. 24th International Symposium on Shock Waves, Beijing Peoples R China, Jul 11-16, 2004. BERLIN: SPRINGER-VERLAG BERLIN. doi: 10.1007/978-3-540-27009-6_41
Capra, B. R., Leyland, P. and Morgan, R. G. (2005). Heat transfer measurements on the first experimental layer of the FIRE II reentry vehicle in expansion tubes. 5th European Symposium on Aerothermodynamics for Space Vehicles, Cologne, Germany, 8-11 November 2004. The Nethelands: ESA Publications.
Hayne, M. J., Mee, D. J., Gai, S. L., Stewart, B. S. and Morgan, R. G. (2004). Flow establishment over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer.
Capra, BR, Morgan, RG and Leyland, W (2004). Heat transfer measurements of the first experimental layer of the fire II reentry vehicle in expansion tubes. 5th European Symposium on Aerothermodynamics for Space Vehicles, Cologne Germany, Nov 08-11, 2004. 2200 AG NOORDWIJK: ESA PUBLICATIONS DIVISION C/O ESTEC.
Capra, B.R., Leyland, P. and Morgan, R.G. (2004). Subscale testing of the FIRE II vehicle in a superorbital expansion tube. 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, U.S.A., 5 - 8 January 2004. United States: American Institute of Aeronautics and Astronautics, AIAA. doi: 10.2514/6.2004-1298
Silvester, T. B. and Morgan, R. G. (2004). Computational hypervelocity aerodynamics of a caret waverider. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Florida, USA, 11-14 July 2004. USA: American Institute of Aeronautics and Astronautics Inc.
Silvester, T. B., Morgan, R. G. and Jacobs, P. A. (2004). Skin friction measurements in a duct in the X3 superorbital expansion tube. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Florida, USA, 11-14 July 2004. USA: American Institute of Aeronautics and Astronautics Inc. doi: 10.2514/6.2004-3551
Ramesh 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
Higgins, 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.
Abdel-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.
Lourel, 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.
Abdel-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.
Inger, 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
Morgan, 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
Stewart, 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.
Lourel, 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
Hayne, 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.
Abdel-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.
Gai, 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
Wegener, 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
Stewart, 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
Hunt 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
Stewart, 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
Morgan 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
Morgan, 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.
Herbrig, 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.
Palmer, 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.
Morgan, R. G. and Stewart, B. S. (1998). The aerodynamic stability of superorbital reentry craft. Monash University.
Kendall, 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.
Morgan 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.
Morgan 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.
Palmer 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.
Sutcliffe 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.
Doolan 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
Stalker, 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
Bakos, 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
Neely, 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
Morgan, RG (1994). Supersonic Combustion Experiments in Free-Piston Reflected Shock Tunnels. Workshop on Combustion, Hampton Va, Oct 12-14, 1992. DORDRECHT: KLUWER ACADEMIC PUBL.
Kendall, 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.
Neely, 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.
Doolan, 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.
Sutcliffe, 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.
Kendall, 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.
Bakos, 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
Buttsworth, 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.
Morgan, 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.
Bakos, RJ and Morgan, RG (1992). Axisymmetric Scramjet Thrust Production. 11th Australasian Fluid Mechanics Conference, Hobart Australia, Dec 14-18, 1992. HOBART: UNIVERSITY TASMANIA.
Neely, 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.
Brescianini, 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
Morris, 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
Morgan, R. G. and Stalker, R. J. (1985). SHOCK TUNNEL MEASUREMENTS OF HEAT TRANSFER IN A MODEL SCRAMJET. Reston, Virigina: AIAA. doi: 10.2514/6.1985-908
Morgan R.G. and Schultz D.L. (1985). INFRARED SCANNING IN TRANSIENT WIND TUNNELS.. Third Australasian Conference on Heat and Mass Transfer., Steering Committee of the Third Australasian Conference on Heat.
Morgan, R. G. and Stalker, R. J. (1985). Heat transfer in a hydrogen scramjet model. Third Australasian Conference on Heat and Mass Transfer., Unknown, Unknown. Steering Committee of the Third Australasian Conference on Heat.
Morgan, R. G. and Stalker, R. J. (1983). EXPERIMENTS ON A SIMPLE SCRAMJET MODEL. Univ of Newcastle.
Department Technical Report
Stennett, S. J., Gildfind, D. E., Jacobs, P. A. and Morgan, R. G. (2018). Operational verification of the X3R facility free-piston driver. 16. School of Mechanical & Mining Engineering, The University of Queensland, Brisbane.
Research Report
Stewart, 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..