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Dr Matthew McGilvray

Honorary Senior Fellow
School of Mechanical and Mining Engineering

Publications

Journal Articles (8)
Conference Papers (23)
Thesis (1)

Journal Articles

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
McGilvray, M., Dann, A. G. and Jacobs, P. A. (2013). Modelling the complete operation of a free-piston shock tunnel for a low enthalpy condition. Shock Waves, 23 (4), 399-406. doi: 10.1007/s00193-013-0437-8
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
McGilvray, Matthew, Kirchhartz, Rainer and Jazra, Thomas (2010). Comparison of mach 10 scramjet measurements from different impulse facilities. AIAA Journal, 48 (8), 1647-1651. doi: 10.2514/1.J050025
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
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

Conference Papers

McGilvray, Matthew , Pearce, William and James, Christopher (2016). Non-Helium Secondary Driver. 7th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Stuttgart, Germany, 21-26 November 2016.
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.
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
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.
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
McGilvray, Matthew, Dann, Andrew G. and Jacobs, Peter A. (2012). Modeling the complete operation of a free-piston shock tunnel for a low enthalpy condition. 28th International Symposium on Shock Waves, Manchester, England, 17 - 22 July 2011. Heidelberg, Germany: Springer. doi: 10.1007/978-3-642-25688-2_107
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
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
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.
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).
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
McGilvray, Matthew, Kirchhartz, Rainer and Jazra, Thomas (2009). Comparison of Mach 10 scramjet measurements from different impulse facilities. 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.
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
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.
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
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
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, 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.
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.
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.
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.

Thesis

Matthew McGilvray (2008). Scramjet testing at high enthalpies in expansion tube facilities. PhD Thesis, School of Engineering, The University of Queensland.