Journal and Conference Publications

Reference papers for Eilmer

These are good to cite if you are using the core gas-dynamics part of the Eilmer code for your own research. Other features of the code (such as the conjugate heat transfer capability) may have separate papers.

  1. Jacobs PA, Gollan RJ. Implementation of a Compressible-Flow Simulation Code in the D Programming Language. Advances of Computational Mechanics in Australia 2016; 846:54-60 (DOI: 10.4028/www.scientific.net/AMM.846.54)
  2. Gollan RJ, Jacobs PA. About the formulation, verification and validation of the hypersonic flow solver Eilmer. International Journal for Numerical Methods in Fluids 2013; 73:19-57 (DOI: 10.1002/fld.3790)

Other papers on development of Eilmer

The following papers are about Eilmer4, Eilmer3, mb_cns code development.

  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 (DOI: doi.org/10.1016/j.compfluid.2016.11.017)
  2. Qin, Kan, Jahn, Ingo, Gollan, Rowan and Jacobs, Peter (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
  3. 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. doi:10.1016/j.jcp.2015.12.004
  4. 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.
  5. 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.
  6. 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, (148-151). 7-9 December 2015.
  7. Jacobs, Peter and Gollan, Rowan (2015). Implementation of a compressible-flow simulation code in the D programming language. In: ACCM2015 2nd Australasian Conference on Computational Mechanics. Australasian Conference on Computational Mechanics, Brisbane, Australia, 30 November to 1 December 2015.
  8. Jahn, Ingo H. J. (2015) Radial inflow turbine meshing rev. 1. Mechanical Engineering Report 2015/03, School of Mechanical and Mining Engineering, The University of Queensland.
  9. Stennett, Samuel, Chan, Wilson, Gildfind, David and Jacobs, Peter (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
  10. Jahn, Ingo H. J. and Qin, Kan (2015) e3prepToFoam: a mesh generator for OpenFOAM. 2015/04, School of Mechanical and Mining Engineering, The University of Queensland.
  11. Jacobs, P. A., Gollan, R. J., Potter, D. F., Zander, F., Gildfind, D. E., Blyton, P., Chan, W. Y. K. and Doherty, L. (2014) Estimation of high-enthalpy flow conditions for simple shock and expansion processes using the ESTCj program and library St Lucia, QLD, Australia.
  12. Gollan RJ, Jacobs PA. (2012) Verification of a hypersonic flow solver. 18th Australasian Fluid Mechanics Conference, Launceston, Tasmania. 2012
  13. Chan WYK, Jacobs PA, Mee DJ. (2012) Suitability of the k-omega turbulence model for scramjet flowfield simulations. International Journal for Numerical Methods in Fluids 2012, Vol 70, Issue 4, pages 493-514; DOI: 10.1002/fld.2699
  14. Goozee RJ, Jacobs PA. (2002) Parallelism for simulations of an entire shock tunnel facility. Computational Fluid Dynamics 2002.
  15. McGhee AM, Jacobs PA. (1995) Parallel computation of hypervelocity flow. Computational Techniques and Applications: CTAC95.
  16. Jacobs PA. (1992) An approximate Riemann solver for hypervelocity flows. AIAA Journal, 1992; 30(10):2558-2561.
  17. Jacobs PA. (1991) Single-block Navier-Stokes integrator. ICASE Interim Report 18, 1991.

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. Submitted to Shock Waves.

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

Reference Presentation for NENZFr

  1. Jacobs PA, Gollan RG and Zander F, Still using NENZF? That’s so 1960s. International Workshop on Shock Tube Technologies, March 2011, The University of Queensland.

Theses associated with or using the codes

These are Masters or PhD theses that have developed parts of the simulation codes or have made use of the codes.

  1. Banerji, Nikhil (2017) The effects of radiation on ablative heat shields during atmospheric entry. PhD Thesis No. 7681 Ecole Polytechnique Federale de Lausanne.
  2. Kang, Xin (2017) Micro/mesoscale combustion based portable power generating system. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  3. Wei, Han (2017) Air radiation in superorbital expanding flow. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  4. Fahy, Elise (2016) Superorbital re-entry shock layers: Flight and laboratory comparisons. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  5. Bevilacqua, Alexandre (2016) Numerical rebuilding of expansion tunnel ablation testing in terrestrial entry conditions. Master of Science and Technology, University of Pierre and Marie Curie and Ecole Polytechnique Federale Lausanne. http://infoscience.epfl.ch/record/225593
  6. Bond, Daryl (2015). Numerical investigation of gaseous heat and mass transfer: the effect of rarefaction. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland. doi:10.14264/uql.2015.511 [used geometry functions only]
  7. Czapla, Jason (2015) Investigation of supersonic impulse turbines for application to geothermal binary power stations. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  8. Porat, Hadas (2015) Measurement of radiative heat transfer in simulated Titan and Mars atmospheres in expansion tubes. PhD Thesis, School of Mechancial and Mining Engineering, The University of Queensland.
  9. Sheikh, Umar (2014) Re-entry radiation aerothermodynamics in the vacuum ultraviolet. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland and Ecole Centrale Paris. doi:10.14264/uql.2014.305
  10. Al-Doori, Ghassan Fadil Lattif (2013) Investigation of refrigeration system steam ejector performance through experiments and computational simulations. PhD Thesis, School of Mechanical and Electrical Engineering, University of Southern Queensland.
  11. Chan, Wilson (2012) Effects of flow non-uniformities on drag reduction by boundary layer combustion. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  12. de Miranda Ventura, Carlos (2012) Aerodynamic design and performance estimation of radial inflow turbines for renewable power generation applications. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  13. O’Flaherty, Brendan (2012) Reducing the global warming potential of coal mine ventilation air by combustion in a free-piston engine. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  14. Gildfind, David (2012) Development of high total pressure scramjet flow conditions using the X2 expansion tube. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland.
  15. Deepak Narayan Ramanath (2011) Computational Studies of Hypersonic High Enthalpy Separated Flows. PhD Thesis, University of New South Wales, Australian Defence Force Academy, School of Engineering and Information Technology.
  16. Kim, Jae Won (2011) Numerical simulation of thermochemical non-equilibrium flow around blunt bodies considering catalytic wall effects. Masters of Science and Engineering Thesis, School of Mechanical, Aerospace and Systems Engineering, Division of Aerospace Engineering, KAIST.
  17. Jacobs, Carolyn (2011) Radiation in low density hypervelocity flows. PhD Thesis, The University of Queensland and Ecole Centrale Paris.
  18. Potter, Daniel (2011) Modelling of radiating shock layers for atmospheric entry at Earth and Mars. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  19. Gollan, Rowan (2009) The computational modelling of high-temperature gas effects with application to hypersonic flows. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland.
  20. Kirchhartz, Rainer (2009) Upstream Wall Layer Effects on Drag Reduction with Boundary Layer Combustion. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.
  21. Window, Adriaan (2008) Simulation of separating flows in the X2 expansion tube over bluff aerocapture vehicles. Master of Philosophy Thesis, School of Engineering, The University of Queensland.
  22. McGilvray, Matthew (2008) Scramjet testing at high enthalpies in expansion tube facilities. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland.
  23. Tang, Joseph (2008) Development of a parallel adaptive cartesian cell code to simulate blast in complex geometries. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland.
  24. Denman, Andrew (2007) Large-eddy simulation of compressible turbulent boundary layers with heat addition. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland.
  25. Scott, Michael (2006) Development and modelling of expansion tubes. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland.
  26. Elford, Michael (2005) Validation of a CFD solver for hypersonic flows. Master of Philosophy Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland.
  27. Stewart, Benjamin (2004) Predicted scramjet testing capabilities of the proposed RHYFL-X expansion tube. PhD Thesis, Division of Mechanical ENgineering, The University of Queensland.
  28. Goozee, Richard (2003) Simulation of a complete shock tunnel using parallel computer codes. PhD Thesis, Division of Mechanical Engineering, School of Engineering, The University of Queensland.
  29. Austin, Kevin (2002) Evolutionary design of robust flight control for a hypersonic aircraft. PhD Thesis, Department of Mechanical Engineering, The University of Queensland.
  30. Wheatley, Vincent (2001) Modelling low-density flow in hypersonic impulse facilities. Masters of Engineering Science Thesis, Department of Mechanical Engineering, The University of Queensland.
  31. Faddy, James (2000) Computational modelling for shock tube flows. Masters of Engineering Science Thesis, Department of Mechanical Engineering, The University of Queensland.
  32. Craddock, Christopher (1999) Computational optimization of scramjets and shock tunnel nozzles. PhD Thesis, Department of Mechanical ENgineering, The University of Queensland.
  33. Johnston, Ian (1999) Simulation of flow around hypersonic blunt-nosed vehicles for the calibration of air data systems. PhD Thesis, Department of Mechanical Engineering, The University of Queensland.
  34. Petrie-Repar, Paul (1997) Numerical simulation of diaphragm rupture. PhD Thesis, Mechanical Engineering Department, The University of Queensland.

Papers on applications of the codes

The following papers have made use, in one way or another, of the flow-simulation codes.

Turbomachinery flows:

  1. Qin, Kan, Jahn, Ingo H. and Jacobs, Peter 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: doi:10.1115/1.4034723
  2. 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.
  3. Qin, Kan, Jahn, Ingo and Jacobs, Peter (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
  4. Qin, Kan, Jahn, Ingo and Jacobs, Peter (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.
  5. Jahn, Ingo and Jacobs, Peter (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
  6. Czapla, Jason Paul (2015). Investigation of supersonic impulse turbines for application to geothermal binary power stations PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland. doi:10.14264/uql.2015.340
  7. 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.
  8. Ventura C, Sauret E, Jacobs PA, Petrie-Repar P, Gollan RG, van der Laan P. (2010) Adaption and use of a compressible flow code for turbomachinery design. 5th European Conference on Computational Fluid Dynamics ECCOMAS CFD 2010, European Community on Computational Methods in Applied Sciences: Lisbon, Portugal, 2010.

Bluff-body and reacting compressible flows:

  1. F Zander, S. Lohle, H. Krag, S. Lemmens, R.J. Gollan and P.A. Jacobs (2017) Numerical flow analysis of the ISS re-entry. 7th European Conference on Space Debris ESA/ESOC, Darmstadt, Germany, April 2017.
  2. Elise Fahy, David Buttsworth, Rowan Gollan, Peter Jacobs, and Richard G. Morgan. (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
  3. Gisu Park, Sudhir L. Gai, and Andrew J. Neely. (2016) Base Flow of Circular Cylinder at Hypersonic Speeds, AIAA Journal, Vol. 54, No. 2, pp. 458-468. http://dx.doi.org/10.2514/1.J054270
  4. Amna Khraibut, Sudhir Gai, and Andrew J. Neely. (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
  5. Zander, F., Gollan, R. J., Jacobs, P. A. and Morgan, R. G. (2014) Hypervelocity shock standoff on spheres in air. Shock Waves, 24 2: 171-178. doi:10.1007/s00193-013-0488-x
  6. 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. DOI http://dx.doi.org/10.6112/kscfe.2013.18.3.087
  7. 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
  8. 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. doi:10.1007/978-3-319-16835-7_85
  9. 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.
  10. 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.
  11. Gollan RJ, Jacobs PA. (2011) On the validation of a hypersonic flow solver using measurements of shock detachment distance. 28th International Symposium on Shock Waves, 2011.
  12. Gisu Park, Sudhir L. Gai, and Andrew J. Neely. (2010) Aerothermodynamics Behind a Blunt Body at Superorbital Speeds, AIAA Journal, Vol. 48, No. 8 (2010), pp. 1804-1816. http://dx.doi.org/10.2514/1.J050251
  13. Potter D, D’Souza M, Morgan R, Jacobs P. (2010) Modelling of an expansion tunnel experiment simulating re-entry of the Hayabusa probe. Proceedings of the 4th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 2010.
  14. McGilvray M, Jacobs PA, Morgan RG, Gollan RJ, Jacobs CM. (2009) Helmholtz resonance of Pitot pressure measurements in impulsive hypersonic test facilities. AIAA Journal 2009; 47(10):2430–2439. (doi:10.2514/1.42543)
  15. Kulkarni V, Kulkarni PS, Reddy KPJ. (2007) Drag reduction by a forward facing aerospike for a large angle blunt cone in high enthalpy flows. 26th International Symposium on Shock Waves, vol. 1, Springer-Verlag, Berlin, Heidelberg: Gottingen, Germany, 2007; 565–570.
  16. Gollan RJ, Jacobs PA. (2004) Computations of Expansion Tube Flows for the Simulation of Planetary Entry. Computational Techniques and Applications Conference, 2004.
  17. Gollan RJ, Jacobs PA, Karl S, Smith SC. (2004) Numerical Modelling of Radiating Superorbital Flows. Australian and New Zealand Industrial and Applied Mathematics Journal, 2004; 45:C248-C268.
  18. Johnston IA, Tuttle SL, Jacobs PA, Shimoda T. (1999) The numerical and experimental simulation of hypervelocity flow around the HYFLEX vehicle forebody. Shock Waves, 1999; 9(1)57-67.
  19. Johnston IA, Jacobs PA, Shimoda T. (1998) A study of flush air data system calibration using numerical simulation. AIAA Journal of Spacecraft and Rockets, 1998; 35(6):812-820.
  20. Johnston IA, Jacobs PA. (1995) Hypersonic blunt body flows in reacting carbon dioxide. Twelfth Australasian Fluid Mechanics Conference, 1995.

Transient ducted flows:

  1. Xin Kang, Rowan J. Gollan, Peter A. Jacobs and Ananthanarayanan Veeraragavan (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
  2. Jimmy-John O.E. Hoste, Vincent Casseau, Marco Fossati, Ian J. Taylor and Rowan J. Gollan (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
  3. Xin Kang, Rowan J. Gollan, Peter A. Jacobs, and Ananthanarayanan Veeraragavan (2017) On the influence of modelling choices on combustion in narrow channels. Computers and Fluids, 144 117-136. doi:10.1016/j.compfluid.2016.11.017
  4. Won Keun Chang, Gisu Park, Yuin Jin, and Jongryul Byun (2016) Shock Impinging Effect on Ethylene Flameholding, Journal of Propulsion and Power, Vol. 32, No. 5 (2016), pp. 1230-1239. http://dx.doi.org/10.2514/1.B36007
  5. 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
  6. 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.
  7. Denman, Zachary J., Chan, Wilson Y. K., Brieschenk, Stefan, Veeraragavan, Ananthanarayanan, Wheatley, Vincent and Smart, Michael 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
  8. Gisu Park, Chul Park, Yuin Jin, Hojin Choi, Jongryul Byun, and Kiyoung Hwang. (2015) Ethylene Transverse Jets in Supersonic Crossflows, Journal of Propulsion and Power, Vol. 31, No. 3, pp. 773-788. http://dx.doi.org/10.2514/1.B35323
  9. 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, (388-391). 7-9 December 2015.
  10. Chan, Wilson Y. K., Mee, David J., Smart, Michael K. and Turner, James 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
  11. 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.
  12. 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. doi:10.2514/6.2014-2953
  13. Denman, Zachary (2013). Modelling Heat Recirculation in Micro-Combustors Using Eilmer3 Honours Thesis, School of Engineering, The University of Queensland.
  14. 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. doi:10.1007/s00193-013-0449-4
  15. Tanimizu K, Mee DJ, Stalker RJ, Jacobs PA. (2011) Thrust nozzle design study for a quasi-axisymmetric scramjet-powered vehicle. AIAA Journal of Propulsion and Power, 2011; 27(1):40-49. (doi: 10.2514/1.48586)
  16. Kirchhartz RM, Mee DJ, Stalker RJ, Jacobs PA, Smart MK. (2010) Supersonic boundary-layer combustion: Effects of upstream entropy and shear-layer thickness. Journal of Propulsion and Power 2010; 26(1):57–66. DOI: 10.2514/1.44485
  17. McGilvray M, Morgan RG, Jacobs PA. (2010) Scramjet experiments in an expansion tunnel: Evaluated using a quasisteady analysis technique. AIAA Journal 2010; 48(8):1635–1646. DOI: 10.2514/1.J050024
  18. Wheatley V, Jacobs PA. (2010) Fuel injection via rectangular cross-section injectors for mixing enhancement in scramjets. 17th Australasian Fluid Mechanics Conference, 2010; Paper 49.
  19. McGilvray M, Morgan RG, Jacobs PA. (2010) Scramjet experiments in an expansion tunnel: Evaluated using a quasi-steady analysis technique. AIAA Journal, 2010; 48(8):1635-1646. (doi: 10.2514/1.51257)
  20. Tanimizu K, Mee DJ, Stalker RJ, Jacobs PA. (2009) Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: theory and experiment. Shock Waves 2009; 19(2):83–93. (doi:10.1007/s00193-009-0194-x)
  21. McGilvray M, Morgan RG, Jacobs PA. (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, 2009. AIAA-Paper-2009-7414
  22. O’Byrne S, Wittig S. (2008) Measurement of hypersonic inlet flow using diode laser absorption spectroscopy. Proceedings of the 8th Australian Space Science Conference, National Space Society of Australia Ltd: Canberra, Australia, 2008; 68–75.
  23. McGilvray M, Jacobs PA, Morgan RG. (2006) Simulations of scramjet starting and establishment time in an expansion tube. 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006. Paper AIAA-2006-8143
  24. Dann A, Denman AW, Jacobs PA, Morgan RG. (2006) Study of separating compressible turbulent boundary-layers. 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006. Paper AIAA-2006-7943
  25. Jacobs PA, Craddock CS. (1999) Simulation and optimization of heated, inviscid flows in scramjet ducts. AIAA Journal of Propulsion and Power, 1999; 15(1):73-81.

Other hypersonic reacting flows (steps, cavities, cones...):

  1. Jokic MD, Buttsworth DR, Balage S (2015) An Aerolance System for Hypersonic Flight. 7th Asia-Pacific International Symposium on Aerospace Technology, 25–27 November 2015, Cairns.
  2. 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
  3. Deepak N.R., Gai S.L., O’ Byrne S., 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.
  4. Khraibut A, Deepak NR, Gai SL, and Neely AJ (2014) Hypersonic Leading Edge Separation. 19th Australasian Fluid Mechanics Conference, Melbourne, Australia, 8-11 December 2014; Paper 80.
  5. O’Byrne S, Gai SL, Deepak NR, Krishna Y, Moss JN (2013) Characterization of a hypersonic low-density flow for separated flow investigations. US Air Force Aerothermodynamics and Turbulence Portfolio Review, July 2013.
  6. Deepak NR, Gai SL and Neely AJ (2013) A computational investigation of laminar shock/wave boundary layer interactions. The Aeronautical Journal, Volume 117, Issue 1187, January 2013, pp. 27-56.
  7. Zander F, Morgan R, Molder S, Jacobs P, Gollan R, Porat H, McIntyre TJ. (2012) Mach disk platform for studying radiating flows. 5th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Barcelona, Spain. 2012
  8. Zander F, Molder S, Morgan R, Jacobs P, Gollan R. (2012) High Temperature Gas Effects for Converging Conical Shocks. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 2012. http://dx.doi.org/10.2514/6.2012-5939
  9. Vikram Sridhar, Sudhir Gai, and Harald Kleine. (2013) Some Numerical Studies of Rectangular Open Cavities at Mach 2”, 19th AIAA/CEAS Aeroacoustics Conference, Aeroacoustics Conferences, (AIAA 2013-2052) http://dx.doi.org/10.2514/6.2013-2052
  10. Deepak NR, Gai SL and Neely AJ. (2012) High-enthalpy flow over a rearward-facing step – a computational study. Journal of Fluid Mechanics 2012; 695:405-438. (doi:10.1017/jfm.2012.29)
  11. Sridhar V, Gai SL, Kleine H (2012) A numerical investigation of supersonic cavity flow at Mach 2. 18th Australasian Fluid Mechanics Conference, Launceston, Australia. Paper 69.
  12. Deepak NR, Gai SL, Neely AJ (2012) High-enthalpy flow over a rearward-facing step - a computational study. Journal of Fluid Mechanics 695:405-438. DOI: 10.1017/jfm.2012.29
  13. Deepak N Ramanath, Sudhir L Gai and Andrew J Neely (2010) Investigation of Heat-Flux in High Enthalpy Hypersonic Flow Over a Rearward-Facing Step. International Journal of Hypersonics 1(2):115-134.
  14. Deepak Narayan Ramanath, Sudhir Gai, and Andrew Neely. (2010) A Computational Study of High Enthalpy Flow Over a Rearward Facing Step, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Aerospace Sciences Meetings, http://dx.doi.org/10.2514/6.2010-444
  15. Deepak NR, Gai SL, Neely AJ (2010) Aerothermodynamics of hypersonic shock wave boundary layer interactions. 17th Australasian Fluid Mechanics Conference, Auckland, New Zealand; Paper 263.
  16. B.H.P. Broksa, W.J.M. Broka, J. Remya, J.J.A.M. van der Mullena, A. Benidarb, L. Biennierb, F. Salamac (2005) Modeling the influence of anode–cathode spacing in a pulsed discharge nozzle. Spectrochimica Acta Part B: Atomic Spectroscopy Volume 60, Issue 11, November 2005, Pages 1442–1449; http://dx.doi.org/10.1016/j.sab.2005.08.012
  17. Sun M, Saito T, Jacobs PA, Timofeev EV, Ohtani K, Takayama K. (2005) Axisymmetric shock wave interaction with a cone: a benchmark test. Shock Waves, 2005; 14(5):313-331.
  18. McGilvray M, Teakle P Jacobs PA, Morgan M. (2005) Geometrical Nozzle Design for Wagtail Rockets. 5th Australian Space Science Conference, 2005.
  19. Denman AJ, Jacobs PA, Mee DJ. (2005) Compressible, Turbulent Flow with Boundary-Layer Heat Addition. 43rd AIAA Aerospace Science Meeting and Exhibit, 2005. AIAA-Paper-2005-1097
  20. Barker P, Bishop A, Littleton B, Jacobs PA. and Rubinsztein-Dunlop, H. (1996) Flow tagging LEI velocimetry of supersonic flow. First Australian Conference on Laser Diagnostics in Fluid Mechanics and Combustion, 1996.

Analysis of expansion-tube facilities:

  1. Toniato, P. and Gildfind, D. and Jacobs, P. 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.
  2. 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 2-16.
  3. 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.
  4. 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. In: 11th International Workshop on Shock Tube Technology, Gottingen, Germany, 30 June -2 July 2016.
  5. Umar A. Sheikh, Richard G. Morgan, and Timothy J. McIntyre. (2016) Optical Thickness Measurements of Vacuum Ultraviolet Radiation in the X2 Expansion Tube. AIAA Journal, Vol. 54, No. 8, pp. 2407-2417. http://dx.doi.org/10.2514/1.J054659
  6. Gildfind, David, Morgan, Richard G. and Jacobs, Peter 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
  7. Burgess, James and Gildfind, David (2015) CFD analysis of early diaphragm removal in expansion tubes. In: Australasian Conference on Computational Mechanics, Brisbane, QLD, Australia, 30 November - 1 December 2015.
  8. Umar A. Sheikh, Richard G. Morgan, and Timothy J. McIntyre. (2015) Vacuum Ultraviolet Spectral Measurements for Superorbital Earth Entry in X2 Expansion Tube. AIAA Journal, Vol. 53, No. 12, pp. 3589-3602. http://dx.doi.org/10.2514/1.J054027
  9. 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
  10. McGilvray, Matthew, Doherty, Luke, Morgan, Richard G. and Gildfind, David 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
  11. 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.
  12. 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, (1-1). 19-24 July 2015.
  13. 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. In: 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, (1-26). 6 - 9 July 2015. doi:10.2514/6.2015-3501
  14. 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.
  15. Andrianatos, Andreas, Gildfind, David and Morgan, Richard (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.
  16. 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. 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.
  17. 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, (83-88). 14-19 July 2013. doi:10.1007/978-3-319-16835-7_11
  18. Jacobs CM, McIntyre TJ, Morgan RG, Brandis AM, Laux CO. (2015) Radiative Heat Transfer Measurements in Low-Density Titan Atmospheres. Journal of Thermophysics and Heat Transfer 29:4, 835-844
  19. Gildfind, David E., James, Chris M., Toniato, Pierpaolo and Morgan, Richard 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
  20. 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.
  21. 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.
  22. 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.
  23. Gildfind, David, Morgan, Richard G., Jacobs, Peter A. and McGilvray, Matthew (2014) Production of high-Mach-number scramjet flow conditions in an expansion tube. AIAA Journal, 52 1: 162-177. doi:10.2514/1.J052383
  24. 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. doi:10.2514/1.A32333
  25. 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. doi:10.2514/6.2013-2647
  26. 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.
  27. 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. doi:10.1007/978-3-319-16835-7_57
  28. 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. doi:10.1007/978-3-319-16835-7_58
  29. 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.
  30. Gildfind DE, Morgan RG, Jacobs PA. (2013) Vibration isolation in a free-piston driven expansion tube facility. Shock Waves 2013; (DOI 10.1007/s00193-013-0433-z)
  31. 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.
  32. Umar Sheikh, Richard Morgan, Fabian Zander, Troy Eichmann, and Tim McIntyre. (2012) Vacuum Ultraviolet Emission Spectroscopy System for Superorbital Re-entries. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, International Space Planes and Hypersonic Systems and Technologies Conferences, http://dx.doi.org/10.2514/6.2012-5807
  33. Jacobs, C. M., McIntyre, T. J., Morgan, R. G., Brandis, A. M. and Laux, C. O. (2012) Radiative heat transfer measurements in low-density titan atmospheres. In: 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, (835-844). 24–28 September 2012. doi:10.2514/1.T4519
  34. Gildfind D, Morgan R, McGilvray M, Jacobs P. (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, 2012.
  35. Gildfind DE, Morgan RG, McGilvray M, Jacobs PA, Stalker RJ, Eichmann TN. (2012) Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions. Shock Waves, 2012; 21(6):559-572.
  36. Gildfind DE, Morgan RG, McGilvray M, Jacobs PA, Stalker RJ, Eichmann TN. (2011) Free-piston driver optimisation for simulation of high Mach number scramjet flow conditions. 28th International Symposium on Shock Waves, 2011.
  37. Gildfind DE, Morgan RG, McGilvray M, Jacobs PA. (2011) High Mach number and total pressure conditions for scramjet testing. 28th International Symposium on Shock Waves, 2011.
  38. McGilvray M, Dann AG, Jacobs PA. (2011) Modeling the complete operation of a free-piston shock tunnel for a low enthalpy condition. 28th International Symposium on Shock Waves, 2011.
  39. Buttsworth DR, Jacobs PA, Potter D, Mudford D, D’Souza M, Eichmann T, Morgan RG, Jenniskens P, McIntyre TJ, Jokic M, Jacobs CM, Upcroft, B, Khan R, Porat H, Neely A. Super-orbital re-entry in Australia –laboratory measurement, simulation and flight observation. 28th International Symposium on Shock Waves, 2011.
  40. Buttsworth, DR, D’Souza M, Potter D, Eichmann T, Mudford N, McGilvray M, McIntyre TJ, Jacobs P, Morgan R. (2010) Expansion Tunnel Radiation Experiments to Support Hayabusa Re-entry Observations. 48th AIAA Aerospace Sciences Meeting, 2010. AIAA-Paper-2010-634.
  41. Jacobs PA, Gollan RJ, Potter DF, Gildfind DE, Eichmann TN, O’Flaherty BT. (2010) CFD Tools for Design and Simulation of Transient Flows in Hypersonic Facilities. RTO-AVT-VKI Lecture Series 2010-AVT186 Aerothermodynamic Design, Review on Ground Testing and CFD, 2010.
  42. McGilvray M, Austin JM, Sharma M, Jacobs PA, Morgan RG. (2009) Diagnostic modelling of an expansion tube operating condition. Shock Waves 2009; 19(1):59–66. (DOI:10.1007/s00193-009-0187-9)
  43. Potter DF, Gollan RJ, Jacobs P, Leyland P. (2008) Numerical simulations and analysis of the 8.5 km/s CO2-N2 EAST shock tube condition. Proceedings of 3rd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry. SP-667, 2008.
  44. Morgan RG, McIntyre TJ, Buttsworth DR, Jacobs PA, Potter DF, Brandis AM, Gollan RJ, Jacobs CM, Capra BR, McGilvray M, Eichmann TN. (2008) Impulse facilities for the simulation of hypersonic radiating flows. 38th Fluid Dynamics Conference and Exhibit, 2008. Paper AIAA-2008-4270
  45. Potter DF, Eichmann T, Brandis A, Morgan RG, Jacobs PA, McIntyre TJ. (2008) Simulation of radiating CO2-N2 shock layer experiments at hyperbolic entry conditions. 40th Thermophysics Conference, 2008. Paper AIAA-2008-3933
  46. Potter DF, Gollan RJ, Eichmann TN, McIntyre TJ, Morgan RG, Jacobs PA. (2008) Simulation of CO2-N2 expansion tunnel flows for the study of radiating shock layers. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008. Paper AIAA-2008-1280
  47. Morgan RG, McIntyre TJ, Jacobs PA, Buttsworth DR, Macrossan MN, Gollan RJ, Capra BR, Brandis AM, Potter D, Eichmann, T, Jacobs CM, McGilvray M, van Diem, D, Scott MP. (2006) Impulse facility simulation of hypervelocity radiating flows. 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 2006. ESA-SP-629
  48. Brandis A, Gollan RJ, Scott M, Morgan RG, Jacobs PA, Gnoffo P. (2006) Expansion tube operating conditions for studying non-equilibrium radiation relevant to Titan aerocapture. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2006. AIAA-Paper-2006-4517
  49. Morgan RG, McIntyre TJ, Gollan RJ, Jacobs PA, Brandis AM, McGilvray M, van Diem D, Gnoffo P, Pulsonetti M, Wright M. (2006) Radiation measurements in nonreflected shock tunnels. 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2006. AIAA-Paper-2006-2958
  50. McGilvray M, Morgan RG, Paull A, Abdel-Jawad MM, Jacobs PA, McIntyre TJ, Scott MA. (2005) Operating condition in UQ’s impulse facilities for scramjet testing. The 25th International Symposium on Shock Waves ISSW25, 2005.
  51. Jacobs PA, Silvester TB, Morgan RG, Scott MP, Gollan RJ, McIntyre TJ. (2005) Superorbital expansion tube operation: Estimates of flow conditions via numerical simulation. 43rd AIAA Aerospace Science Meeting and Exhibit, 2005. AIAA-Paper-2005-0694
  52. Scott MP, Morgan RG, Jacobs PA. (2005) A New Single Stage Driver for the X2 Expansion Tube. 43rd AIAA Aerospace Science Meeting and Exhibit, 2005. AIAA-Paper-2005-0697
  53. Wheatley V, Chiu HS, Jacobs PA, Macrossan MN, Mee DJ, Morgan RG. (2004) Rarefied, superorbital flows in an expansion tube. International Journal of Numerical Methods for Heat & Fluid Flow 2004; 14(4):512–537.
  54. Scott MP, Jacobs PA, Morgan RG. (2004) Nozzle development for an Expansion Tunnel. 24th International Symposium on Shock Waves, Beijing, China, 2004.
  55. Stewart BS, Morgan RG, Jacobs PA. (2003) RocketDyne Hypersonic Flow Laboratory as High Performance Expansion Tube for Scramjet Testing. AIAA Journal of Propulsion and Power, 2003; 19(1):98-103.
  56. Stewart B, Hayne M, Jacobs P, Morgan RG. (2002) Flow establishment in large-scale high-performance expansion tubes. AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, 2002. AIAA-Paper-2002-523
  57. Stewart BS, Morgan RG, Jacobs PA, Austin KJ, Jenkins DM. (2001) Establishment of test conditions in the RHYFL-X facility. 37th AIAA/ASMESAE/ASEE Joint Proplusion Conference and Exhibition 2001. AIAA-Paper-2001-4843
  58. Stewart BS, Jacobs PA, Morgan RG. (2001) The starting process of an expansion tube nozzle. 23rd International Symposium on Shock Waves, 2001. Paper 5456
  59. Stewart B, Morgan RG, Jacobs PA, Jenkins DM. (2000) The RHYFL facility as a high performance expansion tube for scramjet testing. 21st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2000. AIAA-Paper-2000-2595
  60. Kendall MA, Morgan RG, Jacobs PA. (1997) A compact, shock-assisted free-piston driver for impulse facilities. Shock Waves, 1997; 7(4):219-230.
  61. Jacobs PA. (1994) Numerical simulation of transient hypervelocity flow in an expansion tube. Computers and Fluids, 1994; 32(1):77-101.

Analysis of shock tubes, reflected-shock tunnels and gun tunnels:

  1. 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.
  2. Joseph S. Jewell, Christopher C. Huffman, and Thomas J. Juliano. (2017) Transient Startup Simulations for a Large Mach 6 Quiet Ludwieg Tube”, 55th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2017-0743) http://dx.doi.org/10.2514/6.2017-0743
  3. Roger L. Kimmel, Matthew P. Borg, Joseph S. Jewell, KIng-Yiu Lam, Rodney D. Bowersox, Ravi Srinivasan, Steven Fuchs, and Thomas Mooney. (2017) AFRL Ludwieg Tube Initial Performance. 55th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum,(AIAA 2017-0102) http://dx.doi.org/10.2514/6.2017-0102
  4. Klaus Hannemann, Katsuhiro Itoh, David J. Mee, Hans G. Hornung (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.
  5. Denman, Zachary J., Wheatley, Vincent, Smart, Michael K. and Veeraragavan, Ananthanarayanan (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
  6. Luke J. Doherty, Michael K. Smart, and David J. Mee. (2015) Experimental Testing of an Airframe-Integrated Three-Dimensional Scramjet at Mach 10, AIAA Journal, Vol. 53, No. 11 (2015), pp. 3196-3207. http://dx.doi.org/10.2514/1.J053785
  7. 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.
  8. Doherty, Luke J., Smart, Michael K. and Mee, David 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, (3196-3207). 16– 20 June 2014. doi:10.2514/1.J053785
  9. 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. In: Harun Chowdhury and Firoz Alam, Proceedings of the 19th Australasian Fluid Mechanics Conference. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, (60.1-60.4). 8-11 December 2014.
  10. Chan, W. Y. K., Smart, M. K. and Jacobs, P. A. (2014) Experimental validation of the T4 Mach 7.0 nozzle. Technical Report 2014/14, School of Mechanical and Mining Engineering, The University of Queensland.
  11. Gildfind, David E. and Morgan, Richard G. (2014) A new shock tube configuration for studying dust-lifting during the initiation of a coal dust explosion. Journal of Loss Prevention in the Process Industries, 29 1: 198-208. doi:10.1016/j.jlp.2014.02.011
  12. Gisu Park. (2013) Oxygen Catalytic Recombination on Copper Oxide in Tertiary Gas Mixtures”, Journal of Spacecraft and Rockets, Vol. 50, No. 3, pp. 540-555. http://dx.doi.org/10.2514/1.A32312
  13. McGilvray, M., Dann, A. G. and Jacobs, P. A. (2013) Modelling the complete operation of a free-piston shock tunnel for a low enthalpy condition. Shock Waves, 23 4: 399-406. doi:10.1007/s00193-013-0437-8
  14. Chan, W. Y. K., Smart, M. K. and Jacobs, P. A. (2013) Flowpath design of an axisymmetric Mach 7.0 nozzle for T4. Technical Report 2013/02, School of Mechanical and Mining Engineering, The University of Queensland.
  15. Gangurde DY, Mee DJ, Jacobs PA.(2007) Numerical simulation of a Ludwieg-tube fuel delivery system for scramjet experiments in shock tunnels. 16th Australasian Fluid Mechanics Conference, 2007; 645-649.
  16. Gollan RJ, Jacobs CM, Jacobs PA, Morgan RG, McIntyre TJ, Macrossan MN, Buttsworth DR, Eichmann TN, Potter DF. (2007) A simulation technique for radiating shock tube flows. 26th International Symposium on Shock Waves, 2007.
  17. Mundt Ch, Boyce R, Jacobs PA, Hannemann K. (2007) Validation study of numerical simulations by comparison to measurements in piston-driven shock tunnels. Aerospace Science and Technology, 2007; 11:100-109
  18. Buttsworth DR, Goozee RJ, Jacobs PA. (2006) Measurement and simulation of the interface in a low-enthalpy shock tunnel. 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006. Paper AIAA-2006-8108
  19. Goozee RJ, Jacobs PA, Buttsworth DR. (2006) Simulation of a complete reflected shock tunnel showing a vortex mechanism for flow contamination. Shock Waves 2006; 15(3-4):165-176.
  20. Mee DJ, Jacobs PA, Reddy KPJ, Rajakumar B, Arunan E. (2004) Simulation of the performance of a shock tube for studying chemical kinetics. 9th International Workshop on Shock Tube Technology, 2004.
  21. Jacobs PA, Gardner AD, Buttsworth DR, Martinez-Schramm J, Karl S, Hannemann K. (2004) End-to-End Modelling of the HEG Shock Tunnel. 24th International Symposium on Shock Waves, Beijing, China, 2004.
  22. Gardner AD, Jacobs PA, Hannemann K. (2004) End-to-End Modelling and Design of a New Operating Condition for HEG. New Results in Numerical and Experimental Fluid Mechanics IV. Contributions to the 13th STAB/DGLR Symposium Munich, Germany, 2004.
  23. Mundt Ch, Jacobs P, Boyce R. Hannemann K. (2003) A comparative study of piston-driven shock-tunnels. Deutscher Luft- und Raumfahrtkongress, 2003. Paper DGLR-JT-2003-74
  24. Gardner AD, Weiland M, Jacobs PA, Hannemann K. (2002) Extension of the HEG operating conditions for the SHEFEX flight experiment. Thirteenth DGLR-Fach-Symposium der STAB, 2002.
  25. Goozee RJ, Buttsworth DR, Jacobs PA. (2002) Numerical simulation of fluctuations in a shock tunnel flow. Computational Fluid Dynamics 2002.
  26. Buttsworth DR, Jacobs PA, Jones TV. (2002) Simulation of Oxford University Gun Tunnel performance using a quasi-one-dimensional model. Shock Waves, 2002; 11:377-383.
  27. Wendt M, Macrossan M, Jacobs P, Mee D. (1998) Pilot study for a rarefied hypervelocity test facility. 13th Australasian Fluid Mechanics Conference, 1998.
  28. Petrie-Repar PJ, Jacobs PA. (1998) A computational study of shock speeds in high performance shock tubes. Shock Waves, 1998; 8(2):79-91.
  29. Hannemann K, Jacobs PA, Austin JM, Thomas A, McIntyre TJ. (1997) Transient and steady-state flow in a small shock tube. 21st International Symposium on Shock Waves, 1997.
  30. Doolan CJ, Jacobs PA. (1996) Modeling mass entrainment in a quasi-one-dimensional shock tube code. AIAA Journal, 1996; 34(8):1291-1293.
  31. Jacobs PA. (1994) Quasi-one-dimensional modelling of a free-piston shock tunnel. AIAA Journal 1994; 32(1):137-145.
  32. Jacobs PA, Morgan RG, Stalker RJ, Mee DJ. (1993) Use of Argon-Helium Driver-Gas Mixtures in the T4 Shock Tunnel. 19th International Symposium on Shock Waves, Marseille, France, 1993.
  33. Jacobs PA. (1993) Simulation of transient flows in a shock tunnel. Computational Techniques and Applications Conference ‘93, Canberra, Australia, 1993.
  34. Jacobs PA. (1993) Quasi-one-dimensional modelling of free-piston shock tunnels. Aerospace Sciences Meeting, Reno, Nevada, Jan 1993. AIAA-Paper-93-0352.
  35. Jacobs PA, Stalker RJ. (1991) Mach 4 and Mach 8 axisymmetric nozzles for a high-enthalpy shock tunnel. The Aeronautical Journal, 1991; 95(949):324-334.
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