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. (2023)
    Eilmer: an Open-Source Multi-Physics Hypersonic Flow Solver. Computer Physics Communications. Volume 282, 108551. https://doi.org/10.1016/j.cpc.2022.108551

    Short-term share link: https://authors.elsevier.com/c/1fsPB2OInkAiF

  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

2024

  1. Sopek, T., Jacobs, P. A., Subiah, S.-D., Collen, P. and McGilvray, M. (2024) Effect of non-equilibrium thermochemistry on Pitot pressure measurements in shock tunnels (or: Is 0.92 really the magic number?), arXiv:2403.06411, https://doi.org/10.48550/arXiv.2403.06411

  2. Stennett, S., Gildfind, D., Andrianatos, A., Morgan, R., Jacobs, P., James, C., Toniato, P., Chan, W. and Silvester, T. (2024) Large-scale free-piston-driven multi-mode shock expansion tunnel. Experiments in Fluids (2024) 65:16, https://doi.org/10.1007/s00348-023-03756-y

  3. Villodi, N. and Ramachandran, P. (2024) Improved Solid Boundary Treatment for Compressible Smooth Particle Hydrodynamics, arXiv:2402.06231, https://doi.org/10.48550/arXiv.2402.06231

  4. Hyslop, A. and Doherty, L. J. and McGilvray, M. (2023), Comparison of force measurement techniques in a short duration hypersonic facility, Experiments in Fluids, v.65, article 21, https://doi.org/10.1007/s00348-024-03761-9

  5. Gross, T., Torres, E., Schwartzentruber, T. E., Finch, P. M., Girard, J., Schwartz, T., Granowitz, Z., Strand, C. L., Hanson, R. K., Yu, W. M., Austin, J. M. and Hornung, H. (2024), Simulations of Non-Equilibrium Air Chemistry Compared To Hypersonic Wind Tunnel Experiments, AIAA paper 2024-2087, AIAA SCITECH 2024 Forum, https://doi.org/10.2514/6.2024-2087

  6. Pryor, J., Weightman, J., Sandberg, R., Bohon, M. and Edgington-Mitchell, D. M. (2024) A study into the dynamics of an injector-shockwave interaction, AIAA paper 2024-0808, AIAA SCITECH 2024 Forum, https://doi.org/10.2514/6.2024-0808

  7. Steer, J., Clarke, J., McGilvray, M. and Di Mare, L. (2024) LASTA 2.0: Validation of a Reverse Time Integration Method, AIAA paper 2024-0447, AIAA SCITECH 2024 Forum, https://doi.org/10.2514/6.2024-0447

  8. Tapinou, K. C., Jahn, I. Whyborn, L. and Jacobs, P. (2024) Efficient Closely-Coupled Simulations of Hypersonic Fluid–Structure Interaction on an Inclined Ramp in 2-D and 3-D, AIAA paper 2024-1046, AIAA SCITECH 2024 Forum, https://doi.org/10.2514/6.2024-1046

2023

  1. Damm, K. A., Gollan, R. J. and Veeraragavan, A. (2023) Trajectory-based Conjugate Heat Transfer Simulation of the BoLT-II Flight Experiment, AIAA paper 2023-0292, AIAA SCITECH 2023 Forum, https://doi.org/10.2514/6.2023-0292

  2. Damm, K. A., Gibbons, N. N., Jacobs, P. A. and Gollan, R. J. (2023) Application of a Jacobian-Free Newton-Krylov Method to the Simulation of Hypersonic Flows, AIAA paper 2023-2295, AIAA SCITECH 2023 Forum, https://doi.org/10.2514/6.2023-2295

  3. Ogilvie, J. C., Gildfind, D. E., Gollan, R. J. and Gibbons, N. N. (2023) Feasibility of MHD Aerobraking for Use in Martian Atmospheric Entry, AIAA paper 2023-2560, AIAA SCITECH 2023 Forum, https://doi.org/10.2514/6.2023-2560

  4. Whyborn, L. S., Gollan, R. J. and Jacobs, P. A. (2023) Simulation of Multiple Instabilities in the Entropy Layer over a Hypersonic Blunt Cone, AIAA paper 2023-0474, AIAA SCITECH 2023 Forum, https://doi.org/10.2514/6.2023-0474

  5. Finch, P. M., Schwartz, T., Granowitz, Z. N., Yu, W. M., Gross, T., Strand, C. L., Schwartzentruber, T. E., Austin, J. M., Hornung, H. G. and Hanson, R. K. (2023), Near-Body Measurements in Hypersonic Wedge Flows in the T5 Reflected Shock Tunnel by Tunable Diode Laser Absorption Spectroscopy, AIAA paper 2023-2518, AIAA SCITECH 2023 Forum, https://doi.org/10.2514/6.2023-2518

  6. Ravichandran, R., Doherty, L. J., McGilvray, M., Damm, K. A. and Gollan, R. J. (2023) Aerodynamic Effects and Heat Flux Augmentation of a Transpiration Cooled Hypersonic Sharp Leading Edge, AIAA paper 2023-0437, AIAA SCITECH 2023 Forum, https://doi.org/10.2514/6.2023-0437

  7. Steer, J., Collen, P. L., Glenn, A. B., Sopek, T., Hambidge, C., Doherty, L. J., McGilvray, M., Loehle, S. and Walpot, L. (2023) Experimental Study of a Galileo Sub-Scale Model at Ice Giant Entry Conditions in the T6 Free-Piston Driven Wind Tunnel, AIAA paper 2023-1339, AIAA SCITECH 2023 Forum, https://doi.org/10.2514/6.2023-1339

  8. Redding, J., Gamertsfelder, J., Bravo, L. and Khare, P. (2023) Thermochemical non-equilibrium hypersonics flow over a rectangular cavity embedded on a compression ramp, Physics of Fluids, 35(12), https://doi.org/10.1063/5.0172435

  9. Gamertsfelder, J., Redding, J., Bravo, L. and Khare, P. (2023) Flow and Heat Transfer Characteristics of Aerothermodynamic Loading on a Double Cone at Mach 12, Proceedings of ASME 2023 Heat Transfer Summer Conference, Paper HT2023-106391; V001T06A001, https://doi.org/10.1115/HT2023-106391

  10. Jahn, I. H. (2023) Conceptual Study into Wave Ingesting Propulsion for Hypersonic Flight, AIAA paper 2023-3034, 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, https://doi.org/10.2514/6.2023-3034

  11. Jiang, Z. and Chue, R. S. M. (2023) Theories and Technologies of Hypervelocity Shock Tunnels, Cambridge University Press

  12. Schwartz, T., Finch, P. M., Strand, C. L., Hanson, R. K., Luo, Y., Yu, W. M., Austin, J. M. and Hornung, H. (2023) Laser Absorption Sensor Targeting Potassium for Hypersonic Velocity, Temperature, and Enthalpy Measurements, AIAA Journal 61(8), https://doi.org/10.2514/1.J062620

  13. Finch, P. M., Girard, J. J., Strand, C. L., Hanson, R. K., Yu, W. M., Austin, J. M. and Hornung, H. G. (2023), Measurements of T5 Shock Tunnel Freestream Temperature, Velocity, and Composition, AIAA Journal, 61(4), https://doi.org/10.2514/1.J062383

  14. Naved, I., Hermann, T., McGilvray, M., Ewenz-Rocher, M., Hambidge, C., Doherty, L., Le Page, L., Grossman, M. and Vandeperre, L. (2023) Heat Transfer Measurements of a Transpiration-Cooled Stagnation Point in Transient Hypersonic Flow, Journal of Thermophysics and Heat Transfer, 37(2), https://doi.org/10.2514/1.T6610

2022

  1. Hornung, H. G., Gollan, R. J. and Jacobs, P. A. (2022), Computational analysis of experiments on shock detachment in hypersonic flow of nitrogen and carbon dioxide over a wedge, Journal of Fluid Mechanics. 951:A6. https://doi.org/10.1017/jfm.2022.838

  2. Kunze, J., Smart, M. K. and Gollan, R. J. (2022) A Design Method for Three-Dimensional Scramjet Nozzles with Shape Transition, Journal of Propulsion and Power, 38(1), https://doi.org/10.2514/1.B38293

  3. Liu, Y., James, C. M., Morgan, R. G., Jacobs, P. A., Gollan, R. J. and McIntyre, T. J. (2022) Electron Number Density Measurements in a Saturn Entry Condition, AIAA Journal, 60(3), https://doi.org/10.2514/1.J060560

  4. Yunpeng, W. and Jiang, Z. (2022) Theories and methods for designing hypersonic high-enthalpy flow nozzles, Chinese Journal of Aeronautics, 35(1) pp. 318–339, https://doi.org/10.1016/j.cja.2021.01.018

  5. Mecklem, S. A., Landsberg, W. O., Curran, D. and Veeraragavan, A. (2022) Combustion enhancement via tandem cavities within a Mach 8 scramjet combustor, Aerospace Science and Technology, v.124, article 107551, https://doi.org/10.1016/j.ast.2022.107551

  6. Landsberg, W. O., Curran, D. and Veeraragavan, A. (2022), Experimental flameholding performance of a scramjet cavity with an inclined front wall, Aerospace Science and Technology, v.126, article 107622, https://doi.org/10.1016/j.ast.2022.107622

  7. Satchell, M., McGilvrary, M. and Di Mare, L. (2022) Analytical Method of Evaluating Nonuniformities in Shock Tube Flows: Theory and Development, AIAA Journal, 60(2), https://doi.org/10.2514/1.J060990

  8. Gildfind, D. E., Smith, D., Lefevre, A., Jacobs, P. A. and McIntyre, T. J. (2022) Magnetohydrodynamic Aerobraking Shock Stand-Off Measurements with Flight Representative Electrodynamic Boundary Conditions, AIAA Journal, 60(1), https://doi.org/10.2514/1.J060466

  9. Leiser, D., L&oumlhle, S., Zander, F., Buttsworth, D. R., Choudhury, R. and Fasoulas, S. (2022) Analysis of Reentry and Break-Up Forces from Impulse Facility Experiments and Numerical Rebuilding, Journal of Spacecraft and Rockets, 59(4), https://doi.org/10.2514/1.A35204

  10. Lefevre, A., Gildfind, D. E., Gollan, R. J., Jacobs, P. A. and James, C. M. (2022), Magnetohydrodynamic Experiments of Total Heat Flux Mitigation for Superorbital Earth Reentry, AIAA Journal, 60(9), https://doi.org/10.2514/1.J061771

  11. Ewenz Rocher, M., Hermann, T., McGilvray, M. and Gollan, R. J. (2022), Correlation for Species Concentration on a Hypersonic Stagnation Point with Mass Injection, AIAA Journal, 60(5), https://doi.org/10.2514/1.J061159

  12. Gu, S., Olivier, H., Wen, C.-Y., Hao, J. and Wang, Q. (2022) Characterization of reflected shock tunnel air conditions using a simple method, Physics of Fluids, v.34, article 056103, https://doi.org/10.1063/5.0089120

  13. Gu, S., Morgan, R. G., McIntyre, T. J., Brandis, A. M. (2022) An Experimental Study of CO2 Thermochemical Nonequilibrium, AIAA Journal, 60(3), https://doi.org/10.2514/1.J061037

  14. Lefevre, A., Gildfind, D. E., Gollan, R. J., Jacobs, P. A., McIntyre, T. J. and James, C. M. (2022), Experimental Study of Total Heat Flux Mitigation Using Magnetohydrodynamic Flow Control in Superorbital Earth Reentry Flight, AIAA paper 2022-0828, AIAA SCITECH 2022 Forum, https://doi.org/10.2514/6.2022-0828

  15. Satchell, M., Clarke, J., Collen, P. L., McGilvray, M. and di Mare, L. (2022) Advancements in the Modeling and Simulation of Shock Tube Flows, AIAA paper 2022-1638, AIAA SCITECH 2022 Forum, https://doi.org/10.2514/6.2022-1638

  16. Yu, W. M., Austin, J. M. and Hans, H. G. (2022) Freestream Static Pressure Measurements in the T5 Reflected Shock Tunnel, AIAA paper 2022-1658, AIAA SCITECH 2022 Forum, https://doi.org/10.2514/6.2022-1658

  17. Lefevre, A., Gildfind, D. E. and James, C. M. (2022) Coaxial Thermocouple Heat Flux Measurements in Heavily Ionized Flows with Magnetic Fields, Journal of Thermophysics and Heat Transfer, 36(4), https://doi.org/10.2514/1.T6446

2021

  1. Gibbons, N. N., Damm, K. A. and Gollan, R. J. (2021) Flight Regime Limits of a Hypersonic Vehicle using Electron Transpiration Cooling, AIAA paper 2021-4141, ASCEND 2021, https://doi.org/10.2514/6.2021-4141

  2. Gildfind, D. E., Smith, D., Jacobs, P. A., Kelly, R., Lefevre, A. and McIntyre, T. J. (2021) Expansion Tube Test Flow Design for Magnetohydrodynamic Aerobraking, AIAA Journal, 59(4), https://doi.org/10.2514/1.J058389

  3. 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

  4. 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

  5. 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

  6. 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

  7. 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

  8. Girard, J. J., Finch, P. M., Schwartz, T., Yu, W., Strand, C. L., Austin, J. M., Hornung, H. G. and Hanson, R. K. (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

  9. Vanyai, T., Landsberg, W. O., McIntyre, T. J. and Veeraragavan, A. (2021), OH visualization of ethylene combustion modes in the exhaust of a fundamental, supersonic combustor, Combustion and Flame, v.226 pp.143–155, https://doi.org/10.1016/j.combustflame.2020.11.037

  10. Park, S.-H., Kim, J., Choi, I. and Park, G. (2021), Experimental study of separation behavior of two bodies in hypersonic flow, Acta Astronautica, v.181 pp.414–426, https://doi.org/10.1016/j.actaastro.2021.01.037

  11. Kelly, R. M., Gildfind, D. E., McIntyre, T. J. (2021), Emission Spectroscopy of Ionizing Superorbital Expanding Flow, AIAA Journal, 59(8), https://doi.org/10.2514/1.J059345

  12. Lefevre, A., Gildfind, D. E., McIntyre, T. J., Gollan, R. J., Jacobs, P. A. and James, C. M. (2021) Radiative Heat Flux Measurements for Superorbital Earth Re-entries Using an Expansion Tube, AIAA paper 2021-4142, ASCEND 2021, https://doi.org/10.2514/6.2021-4142

  13. Landsberg, W. O., Curran, D. and Veeragavan, A. (2021) Influence of Cavity Depth on Ignition and Flameholding Modes within a Scramjet Combustor, AIAA paper 2021-4162, ASCEND 2021, https://doi.org/10.2514/6.2021-4163

  14. Bone, V. A., Chia, Y. S., Keene, J. C., McQuellin, L. and Jahn, I. H. (2021), Model Predictive Control applied to a Wing-Flap System in Hypersonic (Mach 6) Flow, AIAA paper 2021-1564, AIAA SCITECH 2021 Forum, https://doi.org/10.2514/6.2021-1564

  15. Apirana, S. F., James, C. M., Lewis, S. and Morgan, R. G. (2021), Experimental Methods for Studying Post Shock Relaxation, AIAA paper 2021-0446, AIAA SCITECH 2021 Forum, https://doi.org/10.2514/6.2021-0446

2020

  1. Damm, K. A., Landsberg, W. O., Mecklem, S. and Veeraragavan, A. (2020), Performance analysis and validation of an explicit local time-stepping algorithm for complex hypersonic flows, Aerospace Science and Technology, v.107, article 106321, https://doi.org/10.1016/j.ast.2020.106321

  2. Whyborn, L., Gollan, R. J. and Jacobs, P. A. (2020), Quantitative Comparison of Numerical Errors for High-Speed Flux Schemes, 22nd Australasian Fluid Mechanics Conference, https://doi.org/10.14264/a59731c

  3. Liu, Y., James, C. M., Morgan, R. G. and McIntyre, T. J. (2020) Experimental validation of a test gas substitution for simulating non-equilibrium giant planet entry conditions in impulse facilities, Experiments in Fluids, v.61, article 198, https://doi.org/10.1007/s00348-020-03032-3

  4. 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

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

  6. Trudgian, M. A., Landsberg, W. O. and Veeraragavan, A. (2020) Experimental investigation of inclining the upstream wall of a scramjet cavity, Aerospace Science and Technology, v.99, article 105767, https://doi.org/10.1016/j.ast.2020.105767

  7. Liu, Y., James, C. M., Morgan, R. G. and McIntyre, T. J. (2020) Using Aerothermodynamic Similarity to Experimentally Study Nonequilibrium Giant Planet Entry, Journal of Spacecraft and Rockets, 57(5), https://doi.org/10.2514/1.A34713

  8. Moura, A. F., Gibbons, N. N., Wheatley, V., McIntyre, T. J. and Jahn, I. H. (2020) Characterization of Supersonic Turbulent Combustion in a Mach-10 Scramjet Combustor, AIAA Journal, 58(5), https://doi.org/10.2514/1.J058671

  9. Toniato, P., Gildfind, D. E., Jacobs, P. A. and Morgan, R. G. (2020) Expansion tube nozzle design using a parallel simplex algorithm, Shock Waves, v.30 pp.185–199, https://doi.org/10.1007/s00193-019-00930-2

  10. Hoste, J.-J. O. E., Fechter, S., Karl, S. and Hannemann, K. (2020) Study of a supersonic reacting wall jet with a variable turbulent Prandtl and Schmidt number approach, Aerospace Science and Technology, v.106, article 106070, https://doi.org/10.1016/j.ast.2020.106070

  11. Llobet J. R., Basore K. D., Gollan R. J. and Jahn I. H. (2020), Experimental and numerical heat transfer from vortex-injection interaction in scramjet flowfields, The Aeronautical Journal, 124(1280) pp.1545-1567, https://doi.org/10.1017/aer.2020.39

  12. Mariotto, P., Tibere-Inglesse, A. C., Gollan, R. J., Jacobs, P. A., Perrin, M.-Y. and Laux, C. O. (2020), Atomic State-to-State Modeling of Ionization Nonequilibrium in a Recombining Nitrogen Plasma, AIAA paper 2020-1713, AIAA SCITECH 2020 Forum, https://doi.org/10.2514/6.2020-1713

  13. Convery-Brian, I., Raghunath, S. and Mee, D. J. (2020), Transition-Length Predictions for Hypersonic Flows with an Adverse Pressure Gradient, 22nd Australasian Fluid Mechanics Conference, https://doi.org/10.14264/929d0e1

2019

  1. Gildfind, D.E., Smith, D.R., Lefevre, A., Thompson, O., Jacobs, P.A. , Lewis, S.W., Chia, Y.S., Kelly, R., and McIntyre, T.J. (2019) Progress with Magnetohydrodynamics Experiments at the University of Queensland. Asia Pacific International Symposium on Aerospace Technology, 4-6 December 2019. ISBN 978-1-925627-40-4.

  2. 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, 4-6 December 2019. ISBN 978-1-925627-40-4.

  3. 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.

  4. 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.

  5. Mariotto, P., Tibere-Inglesse, A., McGuire, S., Perrin, M.Y., Laux, C.O., Jacobs, P. and Gollan R. (2019) Vibrational State-to-State Modeling of a Recombining Nitrogen/Argon Plasma. AIAA paper 2019-0796 AIAA SciTech Forum, 7-11 January 2019, San Diego, California.

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.

  4. Gildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. K., and Gollan, R. J. (2018) Scramjet test flow reconstruction for a large-scale expansion tube, Part 1: quasi-one-dimensional modeling. Shock Waves, Vol. 28 pages 877-897, https://doi.org/10.1007/s00193-017-0785-x

  5. Gildfind, D. E., Jacobs, P. A., Morgan, R. G., Chan, W. Y. K., and Gollan, R. J. (2018) Scramjet test flow reconstruction for a large-scale expansion tube, Part 2: axisymmetric-CFD analysis. Shock Waves, Vol. 28 pages 899-918, https://doi.org/10.1007/s00193-017-0786-9

  6. Stennett, S. J. ,Gildfind D. E., Jacobs, P. A. and Morgan, R. G. (2018) Performance Optimization of X3R: A New Reflected Shock Tunnel Mode for the X3 Expansion Tube. AIAA Paper 2018-3563, Aerodynamic Measurement Technology and Ground Testing Conference, June 25-29, 2018, Atlanta, Georgia.

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–air 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. 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.

  10. 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.

  11. 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

2014

  1. Zander, F., Golyylan, R. J., Jacobs, P. A. and Morgan, R. G. (2014) Hypervelocity shock standoff on spheres in air. Shock Waves, 24 2: 171-178. http://dx.doi.org/10.1007/s00193-013-0488-x

  2. Kang, X., Gollan, R. J., Jacobs, P. A. and Veeraragavan, A. (2014). Numerical simulations of premixed combustion in narrow channels. In: Harun Chowdhury and Firoz Alam, The Proceedings of the 19th Australasian Fluid Mechanics Conference. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014.

  3. Denman, Zachary J., Brieschenk, Stefan, Veeraragavan, Anand, Wheatley, Vincent and Smart, Michael K. (2014). Experimental design of a cavity flameholder in a Mach 8 Shape-Transitioning Scramjet. In: 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, United States, (1-11). 16-20 June 2014. http://dx.doi.org/10.2514/6.2014-2953

  4. 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. In: Harun Chowdhury and Firoz Alam, Proceedings of the 19th Australasian Fluid Mechanics Conference. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, (325.1-325.4). 8-11 December 2014.

  5. 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. In: Harun Chowdhury and Firoz Alam, Proceedings of the 19th Australasian Fluid Mechanics Conference. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, (325.1-325.4). 8-11 December 2014.

  6. Gildfind, D. E., James, C. M. and Morgan, R. G. (2014) Performance considerations for expansion tube operation with a shock-heated secondary driver. In: Harun Chowdhury and Firoz Alam, The Proceedings of the 19th Australasian Fluid Mechanics Conference. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, (1-4). 8-11 December 2014.

  7. Gildfind, David, Morgan, Richard G., Jacobs, Peter A. and McGilvray, Matthew (2014) Production of high-Mach-number scramjet flow conditions in an expansion tube. AIAA Journal, 52 1: 162-177. http://dx.doi.org/10.2514/1.J052383

  8. Qin, K., Jahn, I. H. and Jacobs, P. A. (2014). Validation of a three-dimensional CFD analysis of foil bearings with supercritical CO2. In: Harun Chowdhury and Firoz Alam, Proceedings of the 19th Australasian Fluid Mechanics Conference. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, (136.1-136.4). 8-11 December 2014.

2013

  1. Kim JW, Kwon OJ (2013) Numerical simulation of thermochemical non-equilibrium flow around blunt bodies considering catalytic wall effects. J. Comput. Fluids Eng. 18(3):87-93. http://dx.doi.org/10.6112/kscfe.2013.18.3.087

  2. Umar A. Sheikh, Christophe O. Laux, Richard G. Morgan, and Tim J. Mcintyre (2013) Through Surface and Across Surface Vacuum Ultraviolet Spectral Measurements in an Expansion Tube. 44th AIAA Thermophysics Conference, Fluid Dynamics and Co-located Conferences, (AIAA 2013-2644) http://dx.doi.org/10.2514/6.2013-2644

  3. Zander, F., Jacobs, P. A., Gollan, R. J. and Morgan, R. G. (2013). Shock standoff on hemi-spherical bodies in hypervelocity flows. In: Riccardo Bonazza and Devesh Ranjan, 29th International Symposium on Shock Waves 1. International Symposium on Shock Waves (ISSW29), Madison, WI, United States, (539-544). 14-19 July 2013. http://dx.doi.org/10.1007/978-3-319-16835-7_85

  4. Leyland P, McIntyre TJ, Morgan R, Jacobs PA, Zander F, Sheikh U, Eichmann T, Fahy E, Joshi O, Duffa G, Potter D, Banerji N, Mora-Monteros J, Marguet V. (2013) Radiation-ablation coupling for capsule reentry heating via simulation and expansion tube investigations. 5th European Conference for Aeronautics and Space Sciences (EUCASS 2013), Munich, Germany.

  5. Zander F, Jacobs PA, Gollan RJ, Morgan RG. (2013) Shock Standoff on Hemi-Spherical Bodies in Hypervelocity Flows. 29th International Symposium on Shock Waves 2013; Paper 46.

  6. Denman, Zachary (2013). Modelling Heat Recirculation in Micro-Combustors Using Eilmer3 Honours Thesis, School of Engineering, The University of Queensland.

  7. Tanimizu, Katsuyoshi, Mee, David J., Stalker, Raymond J. and Jacobs, Peter A. (2013) Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions. Shock Waves, 23 5: 453-460. http://dx.doi.org/10.1007/s00193-013-0449-4

  8. Capra, Bianca R. and Morgan, Richard G. (2013) Total heat transfer measurements on a flight investigation of reentry environment model. Journal of Spacecraft and Rockets, 50 3: 494-503. http://dx.doi.org/10.2514/1.A32333

  9. 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. In: 44th AIAA Thermophysics Conference 2013: Proceedings. 44th AIAA Thermophysics Conference, San Diego, CA, USA, (377-390). 24-27 June, 2013. http://dx.doi.org/10.2514/6.2013-2647

  10. James, Chris, Gildfind, David, Morgan, Richard G., Jacobs, Peter A. and Zander, Fabian (2013) Designing and simulating high enthalpy expansion tube conditions. In: Proceedings of the 2013 Asia-Pacific International Symposium on Aerospace Technology. APISAT 2013: 2013 Asia-Pacific International Symposium on Aerospace Technology, Takamatsu, Japan, (1-10). 20-22 November 2013.

  11. Gildfind, D. E., Morgan, R. G. and Sancho, J. (2013) Design and commissioning of a new lightweight piston for the X3 Expansion Tube. 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, (367-372). 14-19 July 2013. http://dx.doi.org/10.1007/978-3-319-16835-7_57

  12. Gildfind, D. E., Sancho Ponce, J. and Morgan, R. G. (2013) High Mach Number Scramjet Test Flows in the X3 Expansion Tube. 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, (373-378). 14-19 July 2013. http://dx.doi.org/10.1007/978-3-319-16835-7_58

  13. 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. In: O. Chazot and T. Magin, STO-AVT-VKI Lecture Series Radiation and Gas-Surface Interaction Phenomena in High Speed Re-Entry (2013-AVT-218), Rhode-St-Genèse, Belgium, (5-1-5-65). 6-8 May 2013.

  14. Gildfind DE, Morgan RG, Jacobs PA. (2013) Vibration isolation in a free-piston driven expansion tube facility. Shock Waves 2013; http://dx.doi.org/10.1007/s00193-013-0433-z

  15. McGilvray M, Dann AG, Jacobs PA. (2013) Modelling the complete operation of a free-piston shock tunnel for a low enthalpy condition. Shock Waves 2013; 23(4):399-406.