Journal Articles, Conference Papers and Technical Reports

Reference papers for Eilmer

  1. Gibbons, N. N., Damm, K. A., Jacobs, P. A., and Gollan, R. J. (2022)
    Eilmer: an Open-Source Multi-Physics Hypersonic Flow Solver. Preprint on arXiv. https://doi.org/10.48550/arXiv.2206.01386

  2. Damm, K. A., Gollan, R. J., Jacobs, P. A., Smart, M. K., Lee, S., Kim, E. and Kim, C. (2020) Discrete adjoint optimization of a hypersonic inlet. AIAA Journal, 58(6):2621–2634. https://doi.org/10.2514/1.J058913

  3. Jacobs, P. A. and Gollan, R. J. (2016) Implementation of a Compressible-Flow Simulation Code in the D Programming Language Applied Mechanics and Materials, vol 846, pp. 54-60 (DOI: 10.4028/www.scientific.net/AMM.846.54)

  4. Damm, K. A., Gollan, R. J. and Jacobs, P. A. (2016) Verification of the Least-Squares Procedure within an Unstructured-Grid Flow Solver Presented at 20th Australasian Fluid Mechanics Conference, Perth, 5–8 December, 2016. (DOI: 10.1002/fld.3790)

  5. Gollan, R.J. and Jacobs, P.A. (2013) About the formulation, verificiation and validation of the hypersonic flow solver Eilmer. International Journal for Numercial Methods in Fluids, 73(1):19–57 (DOI: 10.1002/fld.3790)

Reference papers for L1d

  1. Jacobs PA. (1998) Shock tube modelling with L1d. The University of Queensland, Department of Mechanical Engineering Report 13/98, 1998.

  2. Jacobs PA. (1994) Quasi-one-dimensional modelling of a free-piston shock tunnel. AIAA Journal, 1994; 32(1):137-145.

Reference papers for ESTCj and Pitot

These are the Python codes for the calculation of equilibrium shock tube and expansion tube conditions.

  1. Jacobs PA, Gollan RJ, Potter DF, Zander F, Gildfind DE, Blyton P, Chan WYK, Doherty L. (2011) Estimation of high-enthalpy flow conditions for simple shock and expansion processes using the ESTCj program and library. The University of Queensland, Mechanical Engineering Report 2011/02.

  2. James C, Gildfind D, Morgan RG, Jacobs PA and Zander F (2013) Designing and simulating high enthalpy expansion tube conditions. In: Proceedings of the 2013 Asia-Pacific International Symposium on Aerospace Technology, Takamatsu, Japan, (1-10). 20-22 November 2013.

  3. James, CM, Gildfind, DG, Lewis, SW, Morgan, RG, and Zander, F (2017) Implementation of a state-to-state analytical framework for the calculation of expansion tube flow properties. Shock Waves. Online First. DOI 10.1007/s00193-017-0763-3

Reference paper for IMOC

  1. Jacobs PA, Gourlay CM. (1991) An interactive method-of-characteristics program for gas-dynamic calculations. The International Journal of Applied Engineering Education, 1991; 7(3):242-250

Papers contributing to GDTk or applying GDTk

2021

  1. Gildfind, D. E., Smith, D., Lefevre, A., Jacobs, P. A. and McIntyre, T. J. (2021) Magnetohydrodynamic Aerobraking Shock Stand-Off Measurements with Flight Representative Electrodynamic Boundary Conditions, AIAA Journal, article in advance, https://arc.aiaa.org/doi/10.2514/1.J060466

  2. Gu, S., Morgan, R. G., McIntyre, T. J. and Brandis, A. M. (2021) An Experimental Study of CO2 Thermochemical Nonequilibrium, AIAA Journal, article in advance, https://arc.aiaa.org/doi/full/10.2514/1.J061037

  3. Fahy, E. J., Buttsworth, D. R., Gollan, R. J., Jacobs, P. A., Morgan, R. G. and James, C. J. (2021) Experimental and Computational Fluid Dynamics Study of Hayabusa Reentry Peak Heating, AIAA Journal of Spacecraft and Rockets, article in advance, https://doi.org/10.2514/1.A34863

  4. Lefevre, A., Gildfind, D. E., Gollan, R. J., Jacobs, P. A., McIntyre, T. J. and James, C. M. (2021) Expansion Tube Experiments of Magnetohydrodynamic Aerobraking for Superorbital Earth Reentry, AIAA Journal, Vol. 59, No. 8, pp. 3228–3240, https://doi.org/10.2514/1.J060253

  5. Hornung, H. G., Gollan, R. J., Jacobs, P. A. (2021) Unsteadiness boundaries in supersonic flow over double cones, Journal of Fluid Mechanics, Vol. 916, A5, https://doi.org/10.1017/jfm.2021.203

  6. Schwartz, T., Girard, J., Finch, P. M., Yu, W., Lawson, J. M., Strand, C. L., Austin, J. M., Hornung, H. G. and Hanson, R. K. (2021) Characterization of the Caltech Hypervelocity Expansion Tube via Tunable Diode Laser Absorption Spectroscopy, AIAA Paper 2021-3524, https://doi.org/10.2514/6.2021-3524

  7. Girard, J. J., Finch, P. M., Schwartz, T., Strand, C. L., Hanson, R. K., Yu, W. M., Austin, J. M. and Hornung, H. G. (2021) Characterization of the T5 reflected shock tunnel freestream temperature, velocity, and composition using laser absorption spectroscopy, AIAA Paper 2021-3525, https://doi.org/10.2514/6.2021-3525

2020

  1. Yang, Y., Kim, I., and Park, G. (2020) Evaluation of blunt body velocity gradient at the shock tube end-wall. Acta Astronautica, 170 pages 570–576.

  2. Park, S.-H. and Park, G. (2020) Separation process of multi-spheres in hypersonic flow. Advances in Space Research, Vol. 65 pages 392–406.

2019

  1. Kim, I., Park, G., and Na, J. J. (2019) Experimental study of surface roughness effect on oxygen catalytic recombination. International Journal of Heat and Mass Transfer, Vol. 138 pages 916–922.

  2. Kim, K., Park, G., and Jin, S. (2019) Flameholding characteristics of ethylene-fueled model scramjet in shock tunnel. Acta Astronautica, Vol. 161 pages 446–464.

2018

  1. Banerji, N., Leyland, P., Fahy, E., and Morgan, R. (2018) Earth Reentry Flow over a Phenolic Aeroshell in the X2 Expansion Tube. AIAA Journal of Thermophysics and Heat Transfer, 32(2), http://arc.aiaa.org/doi/10.2514/1.T5255

  2. Banerji, N., Leyland, P., Fahy, E. and Morgan, R. (2018) Venus Entry Flow over a Decomposing Aeroshell in X2 Expansion Tube. AIAA Journal of Thermophysics and Heat Transfer, 32(2), http://arc.aiaa.org/doi/10.2514/1.T5172

  3. Chang, W. K., Yang, S., Park, G., and Choi, H. (2018) Ethylene flame-holding in double ramp flows. Aerospace Science and Technology, Vol. 80 pages 413–423.

2017

  1. Kang, X., Gollan, R., Jacobs, P. and Veeraragavan, A. (2017) On the influence of modelling choices on combustion in narrow channels. Computers & Fluids, 144:117–136 http://doi.org/10.1016/j.compfluid.2016.11.017

  2. Kan, Q., Jahn, I. H., and Jacobs, P. A. (2017) Effect of operating conditions on the elastohydrodynamic performance of foil thrust bearings for supercritical CO2 cycles. Journal of Engineering for Gas Turbines and Power, 139(4) http://doi.org/10.1115/1.4034723

  3. Zander, F., Lohle, S., Krag, H., Lemmens, S., Gollan, R. J. and Jacobs, P. A. (2017) Numerical flow analysis of the ISS re-entry. 7th European Conference on Space Debris ESA/ESOC, Darmstadt, Germany, April 2017.

  4. Wei, H., Morgan, R. G., McIntyre, T. J., Brandis, A. M., and Johnston, C. O. (2017) Experimental and Numerical Investigation of Air Radiation in Superorbital Expanding Flow. 47th AIAA Thermophysics Conference, AIAA Paper 2017-4531, https://doi.org/10.2514/6.2017-4531

  5. Kang, X., Gollan, R. J., Jacobs, P. A., and Veeraragavan, A. (2017) Numerical study of the effect of wall temperature profiles on the premixed methane‚Äďair flame dynamics in a narrow channel. RSC Advances, Volume 7 Issue 63 pages 39940-39954. DOI:10.1039/C7RA07265A

  6. Hoste, J.-J. O. E., Casseau, V., Fossati, M., Taylor, I. J. and Gollan, R. J. (2017) Numerical modeling and simulation of supersonic flows in propulsion systems by open-source solvers. 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China. AIAA-Paper-2017-2411

  7. Jewell, J. S., Huffman, C. C. and Juliano, T. J. (2017) Transient Startup Simulations for a Large Mach 6 Quiet Ludwieg Tube. 55th AIAA Aerospace Sciences Meeting, AIAA 2017-0743.

  8. Kimmel, R. L., Borg, M., Jewell, J. S., Lam, K.. Y., Bowersox, R., Srinivasan, R., Fuchs, S., and Mooney, T. (2017) AFRL Ludwieg Tube Initial Performance. 55th AIAA Aerospace Sciences Meeting, AIAA 2017-0102.

  9. Gildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. K., and Gollan, R. J. (2017) Scramjet test flow reconstruction for a large-scale expansion tube, Part 1: quasi-one-dimensional modeling. Shock Waves, Online First, https://doi.org/10.1007/s00193-017-0785-x

  10. Gildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. K., and Gollan, R. J. (2017) Scramjet test flow reconstruction for a large-scale expansion tube, Part 2: axisymmetric-CFD analysis. Shock Waves, Online First, https://doi.org/10.1007/s00193-017-0786-9

  11. Toniato, P., Gildfind, D. E., Jacobs, P. A., and Morgan, R. G. (2017) Optimisation and design of a fully instrumented Mach 12 nozzle for the X3 expansion tunnel. 31st International Symposium on Shock Waves ISSW31, Nagoya, Japan, July 9-14 2017.

  12. Lewis, S. W., Ravichandran, R., Gollan, R. J., Morgan, R. G., Jacobs, P. A., McIntyre, T. J. and Veeraragavan, A. (2017) UQ/AOARD - Rapidly Expanding Nonequilibrium Flows. Annual Report, The University of Queensland, UQ-AOARD-RENF-AN-2017.

  13. Stennett, S., Gildfind, D. and Jacobs, P. (2017) Optimising the X3R reflected shock tunnel free-piston driver for long duration test times. 31st International Symposium on Shock Waves ISSW31, Nagoya, Japan, July 9–14 2017.

2016

  1. Kan, Q., Jahn, I., Gollan, R. J., and Jacobs, P. A. (2016) Development of a computational tool to simulate foil bearings for supercritical CO2 cycles. Journal of Engineering for Gas Turbines and Power, 138(9):092503-1-092503-19. doi:10.1115/1.4032740

  2. Veeraragavan, A., Beri, J. and Gollan, R. J. (2016) Use of the method of manufactured solutions for the verification of conjugate heat transfer solvers. Journal of Computational Physics, 307:308–320. https://doi.org/10.1016/j.jcp.2015.12.004

  3. Damm, K. A., Gollan, R. J. and Veeraragavan, A. (2016) On the effect of workload ordering for reacting flow simulations using GPUs. In: 20th Australasian Fluid Mechanics Conference. 20th Australasian Fluid Mechanics Conference, Perth, Australia, 5–8 December 2016.

  4. Wang, J., Gollan, R. J. and Veeraragavan, A. (2016). Verification of RANS turbulence model in Eilmer using the Method of Manufactured Solutions. In: 20th Australasian Fluid Mechanics Conference. 20th Australasian Fluid Mechanics Conference, Perth, Australia, 5–8 December 2016.

  5. Qin, K., Jahn, I. H. and Jacobs, P. A. (2016). Prediction of dynamic characteristics of foil thrust bearings using computational fluid dynamics. In: 20th Australasian Fluid Mechanics Conference. Australasian Fluid Mechanics Conference, Perth, WA, Australia, 5-8 December 2016.

  6. Qin, K., Jahn, I., and Jacobs, P. A. (2016) Development of a fluid-structure model for gas-lubricated bump-type foil thrust bearings. Applied Mechanics and Materials, 846 169-175. doi:10.4028/www.scientific.net/AMM.846.169

  7. Qin, K., Jahn, I., and Jacobs, P. A. (2016). Effect of operating conditions on the elasto-hydrodynamic performance of foil thrust bearings for supercritical CO2 cycles. In: Proceedings of ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition, Seoul, South Korea, 13-17 June 2016.

  8. Jahn, I. and Jacobs, P. A. (2016) Using meridional streamline and passage shapes to generate radial turbomachinery geometry and meshes. Applied Mechanics and Materials, 846 1-6. doi:10.4028/www.scientific.net/AMM.846.1

  9. Fahy, E., Buttsworth, D., Gollan, R. J., Jacobs, P. A., and Morgan, R. G. (2016) Experimental and Computational Fluid Dynamics Studies of Superorbital Earth Re-entry", 46th AIAA Thermophysics Conference, AIAA AVIATION Forum, (AIAA 2016-3532) http://dx.doi.org/10.2514/6.2016-3532

  10. Park, G., Gai, S. L., and Neely, A. J. (2016) Base Flow of Circular Cylinder at Hypersonic Speeds, AIAA Journal, 54(2):458–468. http://dx.doi.org/10.2514/1.J054270

  11. Banerji, N., Leyland, P., and Morgan, R. G. (2016) Expansion Tunnel Ablation Testing in Venus Entry Conditions, 46th AIAA Thermophysics Conference, AIAA 2016-3231. https://doi.org/10.2514/6.2016-3231

  12. Chang, W. K., Park, G., Jin, Y., and Byun, J. (2016) Shock Impinging Effect on Ethylene Flameholding, Journal of Propulsion and Power, 32(5):1230–1239. http://dx.doi.org/10.2514/1.B36007

  13. Kang, X., Gollan, R., Jacobs, P. A., and Veeraragavan, A. (2016) Suppression of instabilities in a premixed methane-air flame in a narrow channel via hydrogen/carbon monoxide addition. Combustion and Flame, 173:266–275. doi:10.1016/j.combustflame.2016.07.003

  14. Kang, X., Gollan, R. J., Jacobs, P. A., and Veeraragavan, A. (2016) On the effect of outflow boundary truncation for numerical simulation of narrow-channel flames. In: 20th Australasian Fluid Mechanics Conference. 20th Australasian Fluid Mechanics Conference, Perth, Australia, 5–8 December 2016.

  15. Denman, Z. J., Chan, W. Y. K., Brieschenk, S., Veeraragavan, A., Wheatley, V., and Smart, M. K. (2016) Ignition experiments of hydrocarbons in a Mach 8 shape-transitioning scramjet engine. Journal of Propulsion and Power, 32(6):1462–1471. doi:10.2514/1.B36099

  16. 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. In: 20th Australasian Fluid Mechanics Conference. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, Australia, 5–8 December 2016.

  17. Andrianatos, A., Gildfind, D., and Morgan, R. (2016) Preliminary development of high enthalpy conditions for the X3 expansion tube. In: 20th Australasian Fluid Mechanics Conference, 20AFMC, Perth, WA, Australia, 5–8 December 2016.

  18. Toniato, P., Gildfind, D., and Morgan, R. G. (2016) Current progress of the development of a Mach 12 scramjet operating condition in the X3 expansion tube. In: 11th International Workshop on Shock Tube Technology, Gottingen, Germany, 30 June – 2 July 2016.

  19. Sheikh, U. A., Morgan, R. G., and McIntyre, T. J. (2016) Optical Thickness Measurements of Vacuum Ultraviolet Radiation in the X2 Expansion Tube. AIAA Journal, 54(8):2407–2417. http://dx.doi.org/10.2514/1.J054659

  20. Gildfind, D., Morgan, R. G. and Jacobs, P. A. (2016) Expansion tubes in Australia. In Ozer Igra and Friech Seiler (Ed.), Experimental methods of shock wave research (pp. 399-431) Basel, Switzerland: Springer. doi:10.1007/978-3-319-23745-9_13

  21. Cheung, T. M., Schrijer, F. F. J., and Park, G. (2016) Nitrogen Catalytic Recombination on Copper Oxide in Tertiary Gas Mixtures. Journal of Spacecraft and Rockets, 53(4):644–653.

  22. Hannemann, K., Itoh, K., Mee, D. J., and Hornung, H. G. (2016) Free Piston Shock Tunnels HEG, HIEST, T4 and T5. Experimental Methods of Shock Wave Research Volume 9 of the series Shock Wave Science and Technology Reference Library pp 181–264.

  23. Denman, Z. J., Wheatley, V., Smart, M. K. and Veeraragavan, A. (2016) Supersonic combustion of hydrocarbons in a shape-transitioning hypersonic engine. Proceedings of the Combustion Institute, 36(2):2883–2891. doi:10.1016/j.proci.2016.08.081

2015

  1. Damm, K. A., Gollan, R. J. and Veeraragavan, A. (2015). Acceleration of combustion simulations using GPUs. In: Yi Yang and Nigel Smith, The Australian Combustion Symposium 2015 Proceedings. Australian Combustion Symposium, Parkville, VIC, Australia, pp. 148–151. 7–9 December 2015.

  2. Jahn, I. H. J. (2015) Radial inflow turbine meshing rev. 1. Mechanical Engineering Report 2015/03, School of Mechanical and Mining Engineering, The University of Queensland.

  3. Stennett, S. Chan, W., Gildfind, D., and Jacobs, P. A. (2015). Validating the k-omega turbulence model for 3D flows within the CFD solver Eilmer. In: The 2nd Australasian Conference on Computational Mechanics. Australasian Conference on Computational Mechanics, Brisbane, Australia, (67-72). 30 November – 1 December 2015. doi:10.4028/www.scientific.net/AMM.846.67

  4. Jahn, I. H. J. and Qin, K. (2015) e3prepToFoam: a mesh generator for OpenFOAM. 2015/04, School of Mechanical and Mining Engineering, The University of Queensland.

  5. Khraibut, A., Gai, S., and Neely, A. J. (2015) Numerical Investigation of Bluntness Effects on Hypersonic Leading Edge Separation, 53rd AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2015-0984) http://dx.doi.org/10.2514/6.2015-0984

  6. Park, G., Park, C., Jin, Y., Choi, H., Byun, J., and Hwang, K.. (2015) Ethylene Transverse Jets in Supersonic Crossflows, Journal of Propulsion and Power, 31(3):773–788. http://dx.doi.org/10.2514/1.B35323

  7. Kang, X., Gollan, R. J., Jacobs, P. A. and Veeraragavan, A. (2015). Numerical simulation of premixed methane/air flame dynamics in narrow channels. In: Yi Yang and Nigel Smith, The Australian Combustion Symposium 2015 Proceedings. Australian Combustion Symposium, Parkville, VIC, Australia, pp. 388–391. 7–9 December 2015.

  8. Doherty, L. J., Smart, M. K., and Mee, D. J. (2015) Measurement of Three-Components of Force on an Airframe Integrated Scramjet at Mach 10. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, AIAA 2015-3523.

  9. Chan, W. Y. K., Mee, D. J., Smart, M. K., and Turner, J. C. (2015) Drag reduction by boundary-layer combustion: effects of flow disturbances from rectangular-to-elliptical-shape-transition inlets. Journal of Propulsion and Power, 31(5):1256–1267. doi:10.2514/1.B35335

  10. Jokic M. D., Buttsworth D. R., Balage S. (2015) An Aerolance System for Hypersonic Flight. 7th Asia-Pacific International Symposium on Aerospace Technology, 25–27 November 2015, Cairns.

  11. Sridhar V., Gai S. L., Kleine H. (2015) Supersonic Flow over a Rectangular Open Cavity: Effect of Length-to-Depth Ratio. In: Bonazza R., Ranjan D. (eds) 29th International Symposium on Shock Waves 1. Springer, Cham. DOI: 10.1007/978-3-319-16835-7_67

  12. Deepak N. R., Gai S. L., O’Byrne S., and Moss J.N. (2015) Hypersonic High-Enthalpy Flow in a Leading-Edge Separation. In: Bonazza R., Ranjan D. (eds) 29th International Symposium on Shock Waves 1. Springer, Cham.

  13. Khraibut, A., Gai, S. L., and Neely, A. (2015) Numerical Investigation of Bluntness Effects on Hypersonic Leading Edge Separation. 53rd AIAA Aerospace Sciences Meeting, AIAA 2015-0984.

  14. Burgess, J. and Gildfind, D. (2015) CFD analysis of early diaphragm removal in expansion tubes. In: Australasian Conference on Computational Mechanics, Brisbane, QLD, Australia, 30 November – 1 December 2015.

  15. Sheikh, U. A., Morgan, R. G., and McIntyre, T. J. (2015) Vacuum Ultraviolet Spectral Measurements for Superorbital Earth Entry in X2 Expansion Tube. AIAA Journal, 53(12):3589–3602. http://dx.doi.org/10.2514/1.J054027

  16. Gildfind, D. E., James, C. M. and Morgan, R. G. (2015) Free-piston driver performance characterisation using experimental shock speeds through helium. Shock Waves, 25(2):169–176. doi:10.1007/s00193-015-0553-8

  17. McGilvray, M., Doherty, L., Morgan, R. G., and Gildfind, D. E. (2015). T6: The Oxford University Stalker Tunnel. In: 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. International Space Planes and Hypersonic Systems and Technologies Conferences, Glasgow, Scotland, 6-9 July 2015. doi:10.2514/6.2015-3545

  18. James, C., Gildfind, D., Morgan, R, Lewis, S., Fahy, E. and McIntyre, T. (2015). Simulating gas giant entry in an expansion tube. In: 7th Asia-Pacific International Symposium on Aerospace Technology. 7th Asia-Pacific International Symposium on Aerospace Technology, Cairns, Australia, 25–27 November 2015.

  19. James, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W. and McIntyre, T. J. (2015) Simulating Gas Giant Entry with Increased Helium Diluent in in an Expansion Tube. In: Ben-Dor, 30th International Symposium on Shock Waves, Tel Aviv, Israel, 19–24 July 2015.

  20. James, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W., Fahy, E. J. and McIntyre, T. J. (2015) On the current limits of simulating gas giant entry flows in an expansion tube. In: 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6–9 July 2015. doi:10.2514/6.2015-3501

  21. 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. In: 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2–6 March 2015.

  22. Andrianatos, A., Gildfind, D., and Morgan, R. (2015) A study of radiation scaling of high enthalpy flows in expansion tubes. In: 7th Asia-Pacific International Symposium on Aerospace Technology, Cairns, QLD, Australia, 25–27 November 2015.

  23. Toniato, P., Gildfind, D. E., Jacobs, P. A., and Morgan, R. G. (2015) Development of a new Mach 12 scramjet operating capability in the X3 expansion tube. In: 7th Asia-Pacific International Symposium on Aerospace Technology (APISAT). Asia-Pacific International Symposium on Aerospace Technology (APISAT), Cairns, QLD, Australia, 25–27 November 2015.

  24. Morgan, R. G. and Gildfind, D. E. (2015) Shock tube simulation of low Mach number blast waves. In: Riccardo Bonazza and Devesh Ranjan, Proceedings of the 29th International Symposium on Shock Waves (ISSW29). International Symposium on Shock Waves, Madison, WI, United States, 14–19 July 2013. doi:10.1007/978-3-319-16835-7_11

  25. 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. Journal of Thermophysics and Heat Transfer 29(4):835–844.

  26. Gildfind, D. E., James, C. M., Toniato, P., and Morgan, R. G. (2015) Performance considerations for expansion tube operation with a shock-heated secondary driver. Journal of Fluid Mechanics, 777:364–407. doi:10.1017/jfm.2015.349

  27. Wise, D. J. and Smart, M. K. (2015) Experimental Investigation of a Three-Dimensional Scramjet Engine at Mach 12. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, AIAA 2015-3650.

  28. McGilvray, M., Doherty, L. J., Morgan, R. G. and Gildfind, D. E. (2015) T6: The Oxford University Stalker Tunnel. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, AIAA 2015-3545.

  29. Doherty, L. J., Smart, M. K., and Mee, D. J. (2015) Experimental Testing of an Airframe-Integrated Three-Dimensional Scramjet at Mach 10, AIAA Journal, 53(11):3196–3207. http://dx.doi.org/10.2514/1.J053785

  30. Chan, W. Y. K., Smart, M. K. and Jacobs, P. A. (2015) Flowpath design of the Mach 4B nozzle for T4. Technical Report 2015/10, School of Mechanical and Mining Engineering, The University of Queensland.

  31. Doherty, L. J., Smart, M. K. and Mee, D. J. (2015). Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10. In: AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, United States, 16–20 June 2014. doi:10.2514/1.J053785