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Dr Chris James
Dr

Chris James

Email: 
Phone: 
+61 7 336 53783
Mobile: 
0413642000

Overview

Background

Chris James' research is in the fields of experimental hypersonics, hypersonic aerothermodynamics, and planetary entry. His research combines two important and intertwined parts of these fields: the development and understanding of hypersonic test facilities and the performing and analysing of experiments in them. Chris' 28 journal papers, 2 technical notes, and 59 conference publications cover the design, improvement, and simulation of high enthalpy hypersonic facilities such as expansion tubes and shock tunnels, the application and improvement of physical, optical, and radio-based techniques performed on these facilities, non-equilibrium radiation measurements for entry into many planets in the solar system, re-entry observation measurements, and impulse facility ablation testing.

Chris graduated from Mechanical Engineering at UQ in 2012. Following this, he completed his PhD in the Centre for Hypersonics at the University of Queensland (UQ).

During his PhD he developed very high speed Uranus and Saturn entry conditions which were used to perform the fastest experiments which have ever been performed in an expansion tube, as well as developing expansion tube simulation and analysis codes which are now widely used in the Centre for Hypersonics and around the world. He also enrolled in a cotutelle program with École Centrale Paris in Paris, France, and after being awarded an Eiffel Excellence Scholarship by the French government, he passed a year on exchange in Paris, France. In France, Chris was working on developing the capability to perform radiating simulations to support his experimental work at UQ.

Post PhD he was employed in the Centre for Hypersonics helping to develop the X3R reflected shock tunnel, while also supervising and conducting expansion tube research on the X2 expansion tube at UQ.

In 2020, Chris took on a lecturing position for the year and was awarded an Australian Research Council (ARC) DECRA early career fellowship to study Mars return conditions with heated test models at UQ from 2021 to 2023. He was the 2020 recipient of the UQ EAIT Faculty Early Career Researcher Award and in 2021 a paper he presented was awarded the 2021 American Institute of Aeronautics and Astronautics (AIAA) Ground Test Best Paper Award at the 2021 AIAA SciTech Forum.

in 2020 he participated in the University of Southern Queensland (UniSQ) led re-entry observation mission of the Japanese Aerospace Exploration Agency (JAXA) Hayabusa2 re-entry over Woomera, South Australia and in 2022 he led the UQ contingent on the once again UniSQ led re-entry observation mission of the NASA OSIRIS-REx re-entry in the US.

He is now employed at UQ as a UQ Amplify Senior Lecturer where he continues to perform research in giant planet entry through an ARC Discovery Project which he received with his colleague Professor Richard Morgan and continues to develop and improve UQ's X2 expansion tube.

Chris lectures in the School of Mechanical and Mining Engineering at UQ. He lectures both hypersonics and space engineering, covering varied topics such as high temperature gas dynamics, hypersonic test facilities, rarefied gas dynamics, orbital mechanics, rocket trajectories, spacecraft design, spacecraft thermal and power management, and planetary entry.

He has written six popular science article for The Conversation with a more than 200,000 combined reads, and has been interviewed for Youtube and radio many times. He has given invited talks at the University of Oxford and the Engineers Australia Continuing Professional Development seminar series.

Availability

Dr Chris James is:
Available for supervision
Media expert

Qualifications

  • Bachelor of Engineering, The University of Queensland
  • Doctor of Philosophy of Engineering, The University of Queensland

Research interests

  • Planetary entry aerothermodynamics

  • Nonequilibrium hypersonic flows

  • Ablating hypersonic flows

  • Expansion tube facility development and test condition characterisation

  • Improving optical and physical measurement techniques for hypersonic flows

Works

Search Professor Chris James’s works on UQ eSpace

105 works between 2012 and 2025

81 - 100 of 105 works

2018

Conference Publication

Improving high enthalpy expansion tube condition characterisation using high speed imagery

James, Christopher M., Smith, Daniel R., McLean, Carl, Morgan, Richard G., Lewis, Steven W. and Toniato, Pierpaolo (2018). Improving high enthalpy expansion tube condition characterisation using high speed imagery. 34th AIAA Aerodynamic Measurement Technology and Ground Testing Conference 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2018-3805

Improving high enthalpy expansion tube condition characterisation using high speed imagery

2017

Journal Article

Carbon ablation in hypervelocity air and nitrogen shock layers

Lewis, Steven W., James, Christopher M., Ravichandran, Ranjith, Morgan, Richard G. and McIntyre, Timothy J. (2017). Carbon ablation in hypervelocity air and nitrogen shock layers. Journal of Thermophysics and Heat Transfer, 32 (2), 449-468. doi: 10.2514/1.T5270

Carbon ablation in hypervelocity air and nitrogen shock layers

2017

Journal Article

X3 expansion tube driver gas spectroscopy and temperature measurements

Parekh, V., Gildfind, D., Lewis, S. and James, C. (2017). X3 expansion tube driver gas spectroscopy and temperature measurements. Shock Waves, 28 (4), 851-862. doi: 10.1007/s00193-017-0754-4

X3 expansion tube driver gas spectroscopy and temperature measurements

2017

Journal Article

Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in X2

Sheikh, Umar A., Wei, Han, Lewis, Steven W., James, Christopher M., Leyland, Pénélope, Morgan, Richard G. and McIntyre, Timothy J. (2017). Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in X2. AIAA Journal, 55 (12), 1-14. doi: 10.2514/1.J056021

Spectrally filtered imaging and vacuum ultraviolet spectroscopy of preheated models in X2

2017

Journal Article

Carbon ablative shock layer radiation with high surface temperatures

Lewis, Steven W., James, Christopher M., Morgan, Richard G., McIntyre, Timothy J., Alba, Christopher R. and Greendyke, Robert B. (2017). Carbon ablative shock layer radiation with high surface temperatures. Journal of Thermophysics and Heat Transfer, 31 (1), 193-204. doi: 10.2514/1.T4902

Carbon ablative shock layer radiation with high surface temperatures

2017

Conference Publication

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

Geraets, Rowland T. Penty, McGilvray, Matthew, Doherty, Luke J., Morgan, Richard G., James, Christopher M., Vanyai, Tristan and Buttsworth, David R. (2017). Development of a fast-response calorimeter gauge for hypersonic ground testing. AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, CO, United States, 5-9 June 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautic. doi: 10.2514/6.2017-3238

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

2017

Conference Publication

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

Geraets, Rowland T. Penty, McGilvray, Matthew, Doherty, Luke J., Morgan, Richard G., James, Christopher M., Vanyai, Tristan and Buttsworth, David R. (2017). Development of a fast-response calorimeter heat transfer gauge for hypersonic ground testing. 33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Denver, Colorado, 5-9 June 2017. American Institute of Aeronautics and Astronautics Inc, AIAA.

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

2017

Conference Publication

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

James, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W. and McIntyre, T. M. (2017). Simulating gas giant entry with increased helium diluent in an expansion tube. 30th International Symposium on Shock Waves, Tel Aviv, Israel, 19-24 July 2015. Cham, Switzerland: Springer International Publishing. doi: 10.1007/978-3-319-44866-4_104

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

2017

Conference Publication

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

Ravichandran, R., Lewis, S.W., James, C.M., Morgan, R.G. and McIntyre, T.J. (2017). Interaction of ablating carbon with expanding earth entry flows in the X2 expansion tube. 9th Ablation Workshop, Bozeman, MT, United States, 30-31 August 2017.

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

2017

Conference Publication

Experimentally simulating gas giant entry in an expansion tube

James, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W. and McIntyre, Timothy J. (2017). Experimentally simulating gas giant entry in an expansion tube. 21st International Space Planes and Hypersonic Systems and Technologies Conference, Xiamen, China, 6 - 9 March 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-2152

Experimentally simulating gas giant entry in an expansion tube

2016

Conference Publication

Non-Helium Secondary Driver

McGilvray, Matthew , Pearce, William and James, Christopher (2016). Non-Helium Secondary Driver. 7th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, Stuttgart, Germany, 21-26 November 2016.

Non-Helium Secondary Driver

2015

Journal Article

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

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

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

2015

Journal Article

Free-piston driver performance characterisation using experimental shock speeds through helium

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

Free-piston driver performance characterisation using experimental shock speeds through helium

2015

Conference Publication

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

James, C. M., Gildfind, D. E., Morgan, R. G., Lewis, S. W., Fahy, E. J. and McIntyre, T.J. (2015). Limits of Simulating Gas Giant Entry at True Gas Composition and True Flight Velocities in an Expansion Tube. 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2-6 March 2015.

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

2015

Conference Publication

Simulating gas giant entry in an expansion tube

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

Simulating gas giant entry in an expansion tube

2015

Conference Publication

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

Morgan, R., Rees, B., Rutherford, J., Jefferey, M., Sollart, M., Morris, N., Basore, K., James, C., Wei, H., Gu, S., Lewis, S. and Landsberg, W. (2015). Advanced hypersonic vehicle component testing using pre-heated models and infrared scanning. 7th Asia-Pacific International Symposium on Aerospace Technology (APISAT), Cairns, QLD, Australia., 25-27 November, 2015.

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

2015

Conference Publication

Working towards simulating gas giant entry radiation in an expansion tube

James, C .M., Gildfind, D. E., Morgan, R. G. and McIntyre, T. J. (2015). Working towards simulating gas giant entry radiation in an expansion tube. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_89

Working towards simulating gas giant entry radiation in an expansion tube

2015

Conference Publication

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

James, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W., Fahy, Elise J. and McIntyre, Timothy J. (2015). On the current limits of simulating gas giant entry flows in an expansion tube. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6 - 9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3501

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

2015

Conference Publication

X3 expansion tube driver gas spectroscopy and temperature measurements

Parekh, Viha, Gildfind, David, Lewis, Steven and James, Christopher (2015). X3 expansion tube driver gas spectroscopy and temperature measurements. AIAA Australian-Asia Regional Student Conference, Canberra, ACT, Australia, 23-24 November, 2015. American Institute of Aeronautics and Astronautics.

X3 expansion tube driver gas spectroscopy and temperature measurements

2014

Conference Publication

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

Gildfind, D. E., James, C. M. and Morgan, R. G. (2014). Performance considerations for expansion tube operation with a shock-heated secondary driver. 19th Australasian Fluid Mechanics Conference, Melbourne, VIC, Australia, 8-11 December 2014. Melbourne, VIC, Australia: RMIT University.

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

Funding

Current funding

  • 2024 - 2025
    Characterisation and Modelling of Ablative Material Performance (DSP Research Agreement)
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2023 - 2026
    Polymer Matrix Composite Thermal Protection Liners
    Sovereign Manufacturing Automation for Composites CRC
    Open grant
  • 2023 - 2026
    Advancing the Science of Giant Planet Atmospheric Entry
    ARC Discovery Projects
    Open grant
  • 2022 - 2026
    Experimental study of non-equilibrium turbulence-chemistry interaction in external hypersonic flows
    United States Office of Naval Research
    Open grant

Past funding

  • 2024
    Radiation reconstruction for ExoMars capsule flowfield
    AEDS Sarl
    Open grant
  • 2021 - 2024
    Beyond Apollo: The interaction of radiation and ablation during Mars return
    ARC Discovery Early Career Researcher Award
    Open grant
  • 2020 - 2022
    Enhancing the understanding of planetary entry phenomena using additive manufacturing
    Research Donation Generic
    Open grant

Supervision

Availability

Dr Chris James is:
Available for supervision

Before you email them, read our advice on how to contact a supervisor.

Available projects

  • Study of planetary entry flows with radiation and ablation.

    Opportunities always exist for the study of planetary entry in our impulse wind tunnel facilities, either with or without ablation and radiation. These opportunities relate to the particular planetary entry issues which are popular at the time. Currently, these include high speed Earth re-entry which is important for return from Mars in the future, giant planet entry for a planned Uranus or Neptune entry mission, Mars entry at large scale, and Titan entry for an upcoming NASA mission. The phenomena which is studied depends on the particular physical phenomena which is uncertain for the particular scenario. For high speed Earth re-entry, this is the interaction of radiation and ablation, for giant planet entry it is the study of the largely non-equilibrium post-shock flow, for Mars entry it is radiation at low temperatures as seen on the backshell of the vehicle or later in the trajectory, as well as turbulent heating due to the large vehicle sizes, for example. Students with an interest in these topics should contact Dr James directly at c.james4@uq.edu.au for details of specific projects.

Supervision history

Current supervision

Media

Enquiries

Contact Dr Chris James directly for media enquiries about:

  • hypersonics
  • planetary entry
  • space

Need help?

For help with finding experts, story ideas and media enquiries, contact our Media team:

communications@uq.edu.au