OR

Browse By

Professor Richard Morgan

Professor

School of Mechanical and Mining Engineering
Faculty of Engineering, Architecture and Information Technology
r.morgan@uq.edu.au
+61 7 336 53592

Overview

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

View all Publications

Grants

View all Grants

Supervision

View all Supervision

Available Projects

  • Testing of inflatable reentry heat shields

  • Study of aerocapture maneuvers

    Aerocapture is a means of transferring a spacecraft from a hyperbolic to a captive orbit by means of hypervelocity aerodynamic maneuvers. They have great potential to increase the scope of space missions, but have never been tried to date. This project follows on from an initial 2003 study to do an experimental (in X3) and theoretical evaluation of candidate vehicle shapes.

  • Multistage rocket design

    Composite rocket modules developed at UQ will be ready for flight testing in 2004, and are expected to reach speeds of about Mach 3. Future applications anticipate using these modules in a multistaged configuration, and reaching hypersonic speeds. This project involves the design of a multistaged rocket, and the analysis of its expected performance

View all Available Projects

Publications

Book Chapter

  • Experimental investigation of meteorites: ground test facilities

    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

  • Expansion tubes in Australia

    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

  • Radiative heat transfer measurements in a nonreflected shock tube at low pressures

    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

  • Free Piston-Driven Reflected Shock Tunnels

    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.

  • Free piston-Driven expansion tubes

    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 Article

Conference Publication

  • Experimental VUV shock layer radiation measurements for 13 and 14 km/s high speed earth re-entry conditions

    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.

  • Preliminary results for CO2 recombination for low velocity, high density mars aerocapture conditions

    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.

  • Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in X3 Expansion Tunnel

    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

  • Experimental methods for studying post shock relaxation

    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

  • Infrared thermography on a biconic model in Hypersonic expansion tube flows

    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

  • Self-absorption and electron number density measurements on Saturn entry radiation

    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

  • A generalised calibration procedure for performing infrared thermography in expansion tubes

    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

  • Using aerothermodynamic similarity to experimentally study nonequilibrium giant planet entry

    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

  • Development of a fast-response diamond calorimeter heat transfer gauge

    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

  • Infrared thermography in expansion tubes for Martian entry flows

    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

  • Scaled Apollo Heating Testing in a Large Expansion Tube

    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

  • Simulating Uranus Entry in an Expansion Tube

    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

  • The X3R Free-Piston Reflected Shock Tunnel: Australia's New Large-Scale, Long-Duration Hypersonic Testing Capability

    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

  • Testing of ultra fast response, durable co-axial thermocouples for high enthalpy impulse facilities

    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

  • Application of Infrared Thermography in an Expansion Tunnel

    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

  • Commissioning of the T6 Stalker Tunnel

    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

  • Development of a high enthalpy driver in an expansion tube for generating Uranus entry flow conditions

    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.

  • Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnel

    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

  • Driver condition development for high enthalpy operation of the X3 expansion tube

    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

  • Evaluation of electrically insulating coatings for magnetohydrodynamic aerobraking experimentation

    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

  • Expansion tube experiments of graphite ablation and radiation in hypervelocity earth-entry flows

    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.

  • Generating 5-km/s low density hypersonic test flows in an expansion tube for studying ultraviolet radiation

    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

  • Generating High Speed Earth Re-entry Test Conditions in an Expansion Tube for Interplanetary Return Missions

    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

  • Generating high speed earth re-entry test conditions in an expansion tube

    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.

  • Hypervelocity boundary-layer flow with high-temperature surface ablation

    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

  • Multidimensional effects and self- absorption on spectroscopic observations of Saturn entry radiation

    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.

  • Optimisation and design of a fully instrumented Mach 12 nozzle for the X3 expansion tube

    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

  • Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared Thermography

    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

  • Studying post-shock relaxation using a Mach Disk

    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.

  • Testing a full-scale Hayabusa Model in a large expansion tube

    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.

  • The X3R reflected shock tunnel: a new, long-duration operating mode for the X3 expansion tube

    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.

  • Theoretical and experimental study of helium-neon substitution for Saturn entry radiation

    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

  • Experimental analysis of the interaction of carbon and silicon ablation products with expanding hypersonic flows

    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

  • Experimental study of saturn entry radiation with higher amount of diluent in an expansion tube

    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

  • Flow characterization and modeling of the X2 and X3 expansion tubes

    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.

  • Full free-stream mach 12 scramjet testing in expansion tubes

    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

  • Improving high enthalpy expansion tube condition characterisation using high speed imagery

    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

  • Performance optimization of X3R: A new reflected shock tunnel mode for the X3 expansion tube

    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

  • Rapid prototyping in instrumented hypervelocity testing

    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.

  • A new sliding joint to accommodate recoil of a free-piston driven expansion tube

    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

  • Development of a fast-response calorimeter gauge for hypersonic ground testing

    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

  • Development of a fast-response calorimeter heat transfer gauge for hypersonic ground testing

    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.

  • Experimental and numerical investigation of air radiation in superorbital expanding flow

    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

  • Experimentally simulating gas giant entry in an expansion tube

    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

  • Interaction of ablating carbon with expanding earth entry flows in the X2 expansion tube

    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.

  • Preliminary experimental investigation of air radiation in super-orbital expanding flow

    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

  • Simulating gas giant entry with increased helium diluent in an expansion tube

    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

  • Study of afterbody radiation during mars entry in an expansion tube

    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

  • Analysis and rebuilding of experiments on a heated carbon graphite model in the X2 expansion tube

    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

  • Current progress of the development of a Mach 12 scramjet operating condition in the X3 expansion tube

    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.

  • Development of a new Mach 12 scramjet operating capability in the X3 expansion tube

    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.

  • Expansion tunnel ablation testing in venus entry condition

    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

  • Experimental and computational fluid dynamics studies of superorbital earth re-entry

    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

  • Extension of the X3 expansion tube capabilities for Mach 12 scramjet testing: flow condition: development and nozzle optimization

    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.

  • Preliminary development of high enthalpy conditions for the X3 expansion tube

    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.

  • The ESA ARC project: Ablation radiation coupling for hypervelocity re-entry with low density type ablators

    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

  • A study of radiation scaling of high enthalpy flows in expansion tubes

    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.

  • Advanced hypersonic vehicle component testing using pre-heated models and infrared scanning

    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.

  • Comparison of carbon ablative shock-layer radiation with high surface temperatures

    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

  • Design and commissioning of a new lightweight piston for the X3 Expansion Tube

    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

  • Duplication of atmospheric entry in laboratories: what are radiatively coupled flows?

    Morgan, Richard (2015). Duplication of atmospheric entry in laboratories: what are radiatively coupled flows?. International Planetary Probe Workshop, Cologne, Germany, 15-19 June 2015.

  • Emission spectroscopy of a mach disk at Titan atmospheric entry conditions

    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

  • High Mach Number Scramjet Test Flows in the X3 Expansion Tube

    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

  • Hypersonics Research in Australia

    Morgan, Richard (2015). Hypersonics Research in Australia. Air Force Office of Scientific Research, Arlington, VA, United States, 25 March 2015.

  • Intercontinental rocket plane transport network

    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

  • Limits of Simulating Gas Giant Entry at True Gas Composition and True Flight Velocities in an Expansion Tube

    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.

  • Measurements of radiating flow fields in the vacuum ultraviolet

    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

  • On the current limits of simulating gas giant entry flows in an expansion tube

    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

  • Radiative heat transfer measurements in low-density titan atmospheres

    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

  • Radiative heatflux measurements for Titan atmospheric entry condition in superorbital expansion tunnel

    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.

  • Scaled earth re-entry experiments in the X2 expansion tube

    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.

  • Shock standoff on hemi-spherical bodies in hypervelocity flows

    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

  • Shock tube simulation of low Mach number blast waves

    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

  • Simulating gas giant entry in an expansion tube

    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.

  • Study of ablative systems in expansion tubes

    Morgan, Richard (2015). Study of ablative systems in expansion tubes. Ablation Workshop, Tullahoma, TN, United States, 21-22 October 2015.

  • T6: The Oxford University Stalker Tunnel

    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.

  • T6: The Oxford University Stalker Tunnel

    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

  • Transitional and Turbulent Heating in Re-Entry flow, Presentation to the meeting of NATO STO AVT-240 RTG-082 working group on Hypersonic Transition

    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.

  • Working towards simulating gas giant entry radiation in an expansion tube

    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

  • Amplifier design for new CNT radiation gauges in expansion tunnels

    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.

  • Comparison of Titan entry radiation shock-tube data with collisional-radiative models

    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

  • Computational optimisation and analysis of a truncated hypersonic nozzle for X3 expansion tunnel

    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.

  • Design of test flows to investigate binary scaling in high enthalpy CO2-N2 mixtures

    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.

  • Filtered Two-Dimensional Imaging in the X2 Expansion Tube

    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.

  • On the limits of simulating gas giant entry at true gas composition and true flight velocities in an expansion tube

    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.

  • Performance considerations for expansion tube operation with a shock-heated secondary driver

    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.

  • Scaled Hayabusa Experiments in the X2 Expansion Tube

    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.

  • The limits of simulating gas giant entry at true gas composition and true flight velocities in an expansion tube

    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.

  • X3 reflected shock tunnel for extended flow duration

    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.

  • Ablation/radiation studies in the Ecole Centrale plasma torch facility

    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.

  • Characterization of a 50 kW Inductively Coupled Plasma Torch for use in Testing of Ablative Materials

    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.

  • Design, operation and testing in expansion tube facilities for super-orbital re-entry

    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.

  • Designing and simulating high enthalpy expansion tube conditions

    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.

  • Measurements of air plasma/ablator interactions in a 50 kW inductively coupled plasma torch

    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

  • Radiation in low density hypervelocity flows: application to Titan entry

    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.

  • Re-entry radiative heating studies in vacuum ultraviolet

    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.

  • Theoretical validation of a test gas substitution for expansion tube simulation of gas giant entry

    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

  • Through surface and across surface vacuum ultraviolet spectral measurements in an expansion tube

    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

  • Vacuum ultraviolet and ultraviolet emission spectroscopy measurements for Titan and Mars atmospheric entry conditions

    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

  • Vacuum ultraviolet radiation studies in a plasma torch facility

    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.

  • Vacuum ultraviolet radiation studies in a plasma torch facility from 170-200 nm

    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

  • Fast-response pyrometer development for expansion tunnel testing with hot carbon models

    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.

  • Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions

    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

  • High mach number and total pressure flow conditions for scramjet testing

    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

  • High speed imaging of X2 expansion tube flows

    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.

  • High speed imaging of spherical shock standoff in hypervelocity flows

    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.

  • High temperature gas effects for converging conical shocks

    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

  • Hot wall testing methodology for impulse facilities

    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

  • Mach disk platform for studying radiating flows

    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 .

  • Near ultraviolet emission spectroscopy of the Hayabusa re-entry

    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

  • Radiation from simulated atmospheric entry into the gas giants

    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.

  • Radiative heat transfer measurements in a nonreflected shock tube at low pressures

    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.

  • Radiative heat transfer measurements in low density titan atmospheres

    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

  • Simulation of high mach number scramjet flow conditions using the X2 expansion tube

    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

  • Standing shock formation in a non-reflected shock tube

    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

  • Study of hypervelocity non equilibrium flows in impulse facilities

    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

  • Study of radiative heat transfer in titan atmospheric entry

    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.

  • Study of radiative heat transfer in titan atmospheric entry

    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).

  • Toward the full CFD Simulation of expansion tubes

    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.

  • Upgrade of the X3 super-orbital expansion tube

    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.

  • VUV radiation measurements for radiation ablation coupling

    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 .

  • Vacuum ultraviolet emission spectroscopy system for superorbital re-entries

    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

  • Vibration isolation in a free-piston driven Expansion tube

    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.

  • Simulation of radiating flows in impulsive facilities

    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

  • An experimental investigation of radiation over an ablating stardust model at 9.8 KM/S

    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.

  • Analysis of air radiation measurements obtained in the EAST and X2 shocktube facilities

    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).

  • Design of lightweight pistons for the X2 and X3 expansion tube free-piston drivers

    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.

  • Design, construction and testing of sounding rocket payloads at the University of Queensland

    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.

  • Expansion tunnel radiation experiments to support hayabusa re-entry observations

    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

  • Modeling of radiating flows in the atmospheres of the Gas Giants

    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.

  • A simulation technique for radiating shock tube flows

    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

  • Composite scramjet combustor

    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

  • Experimental investigation of the effect of two incident shock waves on a turbulent boundary layer in hypersonic circular duct flows

    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

  • Nonequilibrium radiation modeling and experimentation relevant to titan entry

    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.

  • Overview of radiation intensity measurements on the x2 facility at the university of queensland

    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.

  • Radiation measurements in rarefied Titan atmospheres

    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

  • Radiatively cooled scramjet combustor

    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

  • Scramjet experiments in an expansion tunnel: Evaluated using a quasi- steady analysis technique

    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

  • The generation and measurement of high temperature radiating flows in a high enthalpy pulsed facility

    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.

  • Skin-friction measurements and flow establishment within a long duct at superorbital speeds

    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

  • Impulse facilities for the simulation of hypersonic radiating flows

    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

  • Nonequilibrium radiation intensity measurements in simulated titan atmospheres

    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

  • Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers

    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.

  • Simulation of radiating CO2–N2 shock layer experiments at hyperbolic entry conditions

    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

  • Boundary Layer Transition in an Expansion Tube at a Low Enthalpy Operating Condition

    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

  • CFD designed experiments for shock wave/boundary layer interactions in hypersonic ducted flows

    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.

  • Diagnostic Modelling of an Expansion Tube Operating Condition for a Hypersonic Free Shear Layer Experiment

    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.

  • Experimental study of two-dimensional shock wave/turbulent boundary layer interactions

    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

  • Hypersonics Research in Australia

    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.

  • Nonequilibrium radiation measurements and modelling relevant to Titan entry

    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.

  • Radiation measurements in a simulated non-terrestrial atmosphere

    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.

  • Simulation of CO2–N2 expansion tunnel flow for the study of radiating bluntbody shock layers

    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.

  • Transient Heat Analysis of a Carbon Composite Scramjet Combustion Chamber

    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.

  • Radiative and total heat transfer measurements to a Titan explorer model

    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

  • Simulations of scramjet starting and establishment time in an expansion tunnel

    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

  • Expansion tube operating conditions for studying nonequilibrium radiation relevant to Titan Aerocapture

    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.

  • Impulse facility simulation of hypervelocity radiating flows

    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.

  • Radiation measurements in nonreflected shock tunnels

    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

  • Radiation measurements in nonreflected shock tunnels

    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.

  • Radiative and total heat transfer measurements to a Titan Explorer Model

    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.

  • Simulations of scramjet starting and establishment time in an expansion tunnel

    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.

  • Study of separating compressible turbulent boundary-layers

    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

  • A new single stage driver for the X2 expansion tube

    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

  • Expansion tube investigations of planetary aerodynamics

    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).

  • Flow establishment over rearward-facing steps in high enthalpy flows

    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

  • Geometrical Nozzle Design for Wagtail Rocket Motors

    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.

  • Heat transfer measurements on the first experimental layer of the FIRE II reentry vehicle in expansion tubes

    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.

  • New gauge design to measure radiative heat transfer to a Titan aerocapture vehicle in expansion tubes

    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.

  • Nozzle development for an expansion tunnel

    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

  • Operating conditions in UQ's impulse facilities for scramjet testing

    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.

  • Real gas effects on flows over rearward-facing steps in high enthalpy flows

    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

  • Superorbital expansion tube operation: estimates of flow conditions via numerical simulation

    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

  • Computational hypervelocity aerodynamics of a caret waverider

    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.

  • Flow establishment over rearward-facing steps in high enthalpy flows

    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.

  • Heat transfer measurements of the first experimental layer of the fire II reentry vehicle in expansion tubes

    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.

  • Skin friction measurements in a duct in the X3 superorbital expansion tube

    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

  • Subscale testing of the FIRE II vehicle in a superorbital expansion tube

    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

  • Studies on caret wings at super orbital speeds

    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

  • Shock standoff on hypersonic blunt bodies in multitemperature ionizing nonequilibrium gas flows

    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.

  • A generalized nonequilibrium binary scaling for shock standoff on hypersonic blunt bodies

    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

  • Experimental and numerical studies of flows about a Toroidal Ballute

    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.

  • Heat transfer and flow behind a rearward facing step in a super-orbital expansion tube

    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.

  • Sonic jump for planetary entry vehicles

    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.

  • Sonic line location in reacting flows

    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

  • Stability tests in superorbital expansion tubes

    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.

  • The effect of dissociation on choking of ducted flows

    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

  • The starting processes of an expansion tube nozzle

    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.

  • Transient force measurements at superorbital speeds

    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.

  • Diagnostics of A Range of Highly Superorbital Carbon Dioxide Flows

    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

  • Establishment of test conditions in the RHYFL-X facility

    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

  • Heat transfer behind a step in high enthalpy super-orbital flow

    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

  • Development of X3, A superorbital expansion tube

    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

  • Simulated atmospheric entry ablation in superorbital flows

    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

  • The RHYFL facility as a high performance expansion tube for scramjet testing

    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

  • Ionisation in hypervelocity flows

    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.

  • Simulation of ablative mixing layers in superorbital flows

    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.

  • Total radiative and convective heat transfer to re-entry bodies at superorbital velocities

    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.

  • The aerodynamic stability of superorbital reentry craft

    Morgan, R. G. and Stewart, B. S. (1998). The aerodynamic stability of superorbital reentry craft. Monash University.

  • A review of the use of expansion tubes for creating superorbital flows

    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.

  • A study of free-piston driven double-diaphragm drivers for expansion tubes

    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.

  • Experimental and theoretical investigation of hypervelocity carbon dioxide flows

    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.

  • Mechanical and Space Engineering, a degree for undergraduates

    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.

  • Stagnation point heat transfer in superorbital expansion tubes

    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.

  • A shock tunnel investigation of scramjet performance with partially premixed combustion

    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

  • A two stage free-piston driver for expansion tubes

    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

  • Martian atmospheric entry studies with chemical kinetics in an expansion tube

    Sutcliffe, M. A. and Morgan, R. G. (1994). Martian atmospheric entry studies with chemical kinetics in an expansion tube. IE Aust.

  • High performance, compact free piston driver for shock tubes: practical considerations

    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.

  • Measurement of heating rates for earth entry at 13 kms-1

    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

  • Scramjet combustion and thrust measurements in a reflected shock tunnel with varied test gas atomic oxygen contamination

    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

  • Supersonic Combustion Experiments in Free-Piston Reflected Shock Tunnels

    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.

  • Expansion Tube Simulation of Martian Hypervelocity Aerodynamics

    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.

  • Nonisentropic Shock Tunnel Driver Concepts

    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.

  • Pushing the Edge of the Groundtesting Envelope - the Superorbital Expansion Tube

    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.

  • Test-Time Optimization of a Large-Scale Hypervelocity Expansion Tunnel

    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.

  • A Compound Isentropic Free Piston Driver for Expansion Tunnels

    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.

  • An investigation of a wall-injected scramjet using a shock tunnel

    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

  • Axisymmetric Scramjet Thrust Production

    Bakos, RJ and Morgan, RG (1992). Axisymmetric Scramjet Thrust Production. 11th Australasian Fluid Mechanics Conference, Hobart Australia, Dec 14-18, 1992. HOBART: UNIVERSITY TASMANIA.

  • Effects of oxygen dissociation on hypcrvelocity combustion experiments

    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

  • Flow Measurements and Calibration of a Superorbital Expansion Tube

    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.

  • Shock Interactions with Hypersonic Mixing Layers - Steady Flow Analysis and Experiments

    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.

  • Silane as an ignition aid in scramjets

    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

  • Heat transfer in a hydrogen scramjet model

    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.

  • INFRARED SCANNING IN TRANSIENT WIND TUNNELS.

    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.

  • SHOCK TUNNEL MEASUREMENTS OF HEAT TRANSFER IN A MODEL SCRAMJET

    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

  • EXPERIMENTS ON A SIMPLE SCRAMJET MODEL

    Morgan, R. G. and Stalker, R. J. (1983). EXPERIMENTS ON A SIMPLE SCRAMJET MODEL. Univ of Newcastle.

Edited Outputs

  • Proceedings of the 16th Australasian Fluid Mechanics Conference

    Peter Jacobs, Peter McIntyre, Matthew Cleary, David Buttsworth, David Mee, Rose, Clements, Richard Morgan and Charles Lemckert eds. (2007). Proceedings of the 16th Australasian Fluid Mechanics Conference. 16th Australasian Fluid Mechanics Conference, Gold Coast, QLD Australia, 3-7 December 2007. Brisbane, QLD Australia: The University of Queensland.

Other Outputs

Grants (Administered at UQ)

PhD and MPhil Supervision

Current Supervision

Completed Supervision

Possible Research Projects

Note for students: The possible research projects listed on this page may not be comprehensive or up to date. Always feel free to contact the staff for more information, and also with your own research ideas.

  • Testing of inflatable reentry heat shields

  • Study of aerocapture maneuvers

    Aerocapture is a means of transferring a spacecraft from a hyperbolic to a captive orbit by means of hypervelocity aerodynamic maneuvers. They have great potential to increase the scope of space missions, but have never been tried to date. This project follows on from an initial 2003 study to do an experimental (in X3) and theoretical evaluation of candidate vehicle shapes.

  • Multistage rocket design

    Composite rocket modules developed at UQ will be ready for flight testing in 2004, and are expected to reach speeds of about Mach 3. Future applications anticipate using these modules in a multistaged configuration, and reaching hypersonic speeds. This project involves the design of a multistaged rocket, and the analysis of its expected performance

  • Mars gravity soft landing system

    Involves the design, construction and testing of a full scale impact attenuation system to protect the Mars gravity payload of 15 mice when they land at Woomera. Suitable for group thesis or design project (Mech 4552).

  • Mars gravity entry subsystem

    Involves dynamic and thermal analysis of the Mars Gravity reentry capsule. Suitable for group thesis or design project (Mech 4552). May be split into 2 individual projects.

  • Mars Gravity descent subsystem

    Involves the design, construction and testing of a mortar system for deploying the drogue parachute of the Mars gravity return capsule.

  • Expansion tube performance enhancement

    Expansion tubes use a cascade of shock tubes in series to improve performance over conventional shock tunnels. In general, for 'low' speed applications (less than about 8 km/sec), two tubular sections are optimum.

    However, due to certain restrictions on the operating conditions which are useable, there may be situations where three tubes are better at lower speeds. This thesis invovles a theoretical and experiemntal investigation

    of this effect.

  • Development of improved rupture diaphragms for X3

  • Design, construction and flight testing of Mach 2 ramjet

    Involves the design and construction of all components of a liquid fuel ramjet. Follow on from 2003 flight test at Woomera, October 2003. To be used as project/example material in M&S course work including Aerospace Propulsion, Hypersonics, CFD, Space Enginerring and design. Suitable for group thesis or design project (Mech 4552). Dependent on budget support from School of Engineering.

  • Design, construction and flight testing of Mach 2 pulse detonation wave engine (PDE)

    Involves the design and construction of all components of a PDE. Follow on from 2003 flight test at Woomera (postponed), October 2003. To be used as project/example material in M&S course work including Aerospace Propulsion, Hypersonics, CFD, Space Enginerring and design. Suitable for group thesis or design project (Mech 4552). Dependent on budget support from School of Engineering

  • Design of flight version of a Hybrid rocket

    In 2003, a static hybrid rocket was built and tested by a 4th year M&S student. The project will be extended in 2004 to the development of a flight version of the rocket, with the objective of testing at Woomera in 2005. This project could be run as group design (Mech4552) or a group thesis project.

  • Design and test of a parachute recovery system for the Ausroc 2.5 rocket

  • Commissioning of fibre winding machine for composite pressure vessels

    In 2003, UQ acquired a large fibre winding machine from ASRI/DSTO which can be used for the fabrication of various highly stressed components, including rocket motors, fuel tanks and fire extinguisher cases. This machine needs to be commissioned, programmed and used to prepare prototype fuel tanks fro the ASRI 'Ausroc 2.5' rocket project. The machine is currently configured for mechanical control, and the project involves conversion to computerised fibre positioning.

For Media assistance please contact The Office of Marketing and Communications, (07) 3365 1120

Links

ResearcherID: C-8822-2013

ORCID: 0000-0003-3625-9180

Scopus ID: 7403330181

Personal Profile: Link

Unit Links
Other Media

Related Resources

Similar Staff
Researchers in Associated Units
Fields of Research