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2020 Conference Publication Scaled Apollo Heating Testing in a Large Expansion TubeJames, 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 |
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2020 Conference Publication The X3R Free-Piston Reflected Shock Tunnel: Australia's New Large-Scale, Long-Duration Hypersonic Testing CapabilityStennett, 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 |
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2020 Journal Article Correction: Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in x2 (AIAA Journal, (2017), 55, 12, (4167-4180), 10.2514/1.J056021)Sheikh, Umar A., Wei, Han, Lewis, Steven W., James, Christopher M., Leyland, Pénélope, Morgan, Richard G. and McIntyre, Timothy J. (2020). Correction: Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in x2 (AIAA Journal, (2017), 55, 12, (4167-4180), 10.2514/1.J056021). AIAA Journal, 58 (11), AU2-AU2. doi: 10.2514/1.J056021.c1 |
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2020 Conference Publication Development of a fast-response diamond calorimeter heat transfer gaugeGeraets, 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 |
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2020 Conference Publication Infrared thermography in expansion tubes for Martian entry flowsRamesh, 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 |
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2019 Journal Article Expansion tube nozzle design using a parallel simplex algorithmToniato, P., Gildfind, D. E., Jacobs, P. A. and Morgan, R. G. (2019). Expansion tube nozzle design using a parallel simplex algorithm. Shock Waves, 30 (2), 185-199. doi: 10.1007/s00193-019-00930-2 |
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2019 Conference Publication Testing of ultra fast response, durable co-axial thermocouples for high enthalpy impulse facilitiesJames, 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 |
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2019 Journal Article Filtered image thermography for high temperatures in hypersonic preheated ablation experimentsRavichandran, Ranjith, Buttsworth, David R., Lewis, Steven W., Morgan, Richard G. and McIntyre, Timothy J. (2019). Filtered image thermography for high temperatures in hypersonic preheated ablation experiments. Journal of Thermophysics and Heat Transfer, 33 (4), 1074-1084. doi: 10.2514/1.T5629 |
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2019 Journal Article Simulating gas giant atmospheric entry using helium and neon test gas substitutionsJames, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W. and McIntyre, Timothy J. (2019). Simulating gas giant atmospheric entry using helium and neon test gas substitutions. Journal of Spacecraft and Rockets, 56 (3), 725-743. doi: 10.2514/1.a34282 |
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2019 Journal Article Rapid prototyping for hypervelocity impulse facility test modelsApirana, Steven F. T., James, Christopher M., Eldridge, Robert, Morgan, Richard G. and Lewis, Steven W. (2019). Rapid prototyping for hypervelocity impulse facility test models. Aerospace Science and Technology, 88, 174-184. doi: 10.1016/j.ast.2019.03.024 |
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2019 Conference Publication Testing a full-scale Hayabusa Model in a large expansion tubeAndrianatos, 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. |
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2019 Conference Publication Theoretical and experimental study of helium-neon substitution for Saturn entry radiationLiu, 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 |
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2019 Conference Publication Studying post-shock relaxation using a Mach DiskApirana, 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. |
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2019 Conference Publication Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared ThermographyRamesh, 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 |
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2019 Conference Publication Generating high speed earth re-entry test conditions in an expansion tubeJames, 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. |
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2019 Conference Publication Generating 5-km/s low density hypersonic test flows in an expansion tube for studying ultraviolet radiationThompson, 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 |
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2019 Conference Publication Application of Infrared Thermography in an Expansion TunnelCullen, 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 |
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2019 Conference Publication Development of a high enthalpy driver in an expansion tube for generating Uranus entry flow conditionsThompson, 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. |
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2019 Conference Publication Generating High Speed Earth Re-entry Test Conditions in an Expansion Tube for Interplanetary Return MissionsJames, 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 |
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2019 Conference Publication Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnelCullen, 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 |
