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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

103 works between 2012 and 2025

61 - 80 of 103 works

2019

Conference Publication

Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnel

Cullen, T. G., James, C. M., Gollan, R. J. and Morgan, R. G. (2019). Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnel. 31st International Symposium on Shock Waves, Nagoya, Japan, 9-14 July 2017. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-91017-8_24

Development of a total enthalpy and Reynolds number matched Apollo re-entry condition in the X2 expansion tunnel

2019

Conference Publication

Expansion tube experiments of graphite ablation and radiation in hypervelocity earth-entry flows

Ravichandran, R., Lewis, S.W., James, C.M., Morgan, R.G. and McIntyre, T.J. (2019). Expansion tube experiments of graphite ablation and radiation in hypervelocity earth-entry flows. 8th International Workshop on Radiation of High Temperature Gases, Madrid, Spain, 25-29 March 2019.

Expansion tube experiments of graphite ablation and radiation in hypervelocity earth-entry flows

2019

Conference Publication

The X3R reflected shock tunnel: a new, long-duration operating mode for the X3 expansion tube

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 (APISAT 2019), Gold Coast, QLD, Australia, 4-6 December 2019.

The X3R reflected shock tunnel: a new, long-duration operating mode for the X3 expansion tube

2019

Conference Publication

Theoretical and experimental study of helium-neon substitution for Saturn entry radiation

Liu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy (2019). Theoretical and experimental study of helium-neon substitution for Saturn entry radiation. AIAA Aviation 2019 Forum, Dallas, TX United States, 17-21 June 2019. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3134

Theoretical and experimental study of helium-neon substitution for Saturn entry radiation

2019

Conference Publication

Using a Simplified Canny Edge Detector to Detect Shock Arrival in Expansion Tubes and Shock Tunnels

James, Christopher M. (2019). Using a Simplified Canny Edge Detector to Detect Shock Arrival in Expansion Tubes and Shock Tunnels. 32nd International Symposium on Shock Waves (ISSW32 2019), Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0031-cd

Using a Simplified Canny Edge Detector to Detect Shock Arrival in Expansion Tubes and Shock Tunnels

2019

Conference Publication

Generating High Speed Earth Re-entry Test Conditions in an Expansion Tube for Interplanetary Return Missions

James, Christopher M., Lewis, Steven W., Gildfind, David E., Morgan, Richard G., McIntyre, Timothy J. and Liu, Yu (2019). Generating High Speed Earth Re-entry Test Conditions in an Expansion Tube for Interplanetary Return Missions. 32nd International Symposium on Shock Waves (ISSW32 2019), Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0424-cd

Generating High Speed Earth Re-entry Test Conditions in an Expansion Tube for Interplanetary Return Missions

2019

Conference Publication

Generating 5-km/s low density hypersonic test flows in an expansion tube for studying ultraviolet radiation

Thompson, Matthew, James, Christopher M., Lewis, Steven W., Gildfind, David E. and Morgan, Richard G. (2019). Generating 5-km/s low density hypersonic test flows in an expansion tube for studying ultraviolet radiation. 32nd International Symposium on Shock Waves, Singapore, 14-19 July 2019. Singapore: ISSW. doi: 10.3850/978-981-11-2730-4_0337-cd

Generating 5-km/s low density hypersonic test flows in an expansion tube for studying ultraviolet radiation

2019

Conference Publication

Application of Infrared Thermography in an Expansion Tunnel

Cullen, T., James, C., Gollan, R. and Morgan, R. (2019). Application of Infrared Thermography in an Expansion Tunnel. In: Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019). 32nd International Symposium on Shock Waves (ISSW32 2019), Singapore, (1139-1165). 14-19 July 2019. doi:10.3850/978-981-11-2730-4_0271-cd

Application of Infrared Thermography in an Expansion Tunnel

2019

Conference Publication

Multidimensional effects and self- absorption on spectroscopic observations of Saturn entry radiation

Liu, Yu, Toniato, Pierpaolo, James, Chris, Morgan, Richard and McIntyre, T.J. (2019). Multidimensional effects and self- absorption on spectroscopic observations of Saturn entry radiation. 11th Asia-Pacific International Symposium on Aerospace Technology, Gold Coast, Australia, 4-6 December 2019. Gold Coast, Australia: Engineers Australia.

Multidimensional effects and self- absorption on spectroscopic observations of Saturn entry radiation

2019

Conference Publication

Development of a high enthalpy driver in an expansion tube for generating Uranus entry flow conditions

Thompson, M., James, C.M. and Morgan, R.G. (2019). Development of a high enthalpy driver in an expansion tube for generating Uranus entry flow conditions. 11th Asia-Pacific International Symposium on Aerospace Technology, Gold Coast, Australia, 4-6 December 2019. Gold Coast, Australia: Engineers Australia.

Development of a high enthalpy driver in an expansion tube for generating Uranus entry flow conditions

2018

Journal Article

Calculating shock arrival in expansion tubes and shock tunnels using Bayesian changepoint analysis

James, Christopher M., Bourke, Emily J. and Gildfind, David E. (2018). Calculating shock arrival in expansion tubes and shock tunnels using Bayesian changepoint analysis. Experiments in Fluids, 59 (6) 92. doi: 10.1007/s00348-018-2546-8

Calculating shock arrival in expansion tubes and shock tunnels using Bayesian changepoint analysis

2018

Journal Article

Improved test time evaluation in an expansion tube

James, Christopher M., Cullen, Timothy G. , Wei, Han, Lewis, Steven W., Gu, Sangdi, Morgan, Richard G. and McIntyre, Timothy J. (2018). Improved test time evaluation in an expansion tube. Experiments in Fluids, 59 (5) 87. doi: 10.1007/s00348-018-2540-1

Improved test time evaluation in an expansion tube

2018

Journal Article

Implementation of a state-to-state analytical framework for the calculation of expansion tube flow properties

James, C. M., Gildfind, D. E., Lewis, S. W., Morgan, R. G. and Zander, F. (2018). Implementation of a state-to-state analytical framework for the calculation of expansion tube flow properties. Shock Waves, 28 (2), 349-377. doi: 10.1007/s00193-017-0763-3

Implementation of a state-to-state analytical framework for the calculation of expansion tube flow properties

2018

Conference Publication

Magnetohydrodynamic drag force measurements in an expansion tube

Smith, Daniel R., Gildfind, David E., James, Christopher M., McIntyre, Timothy J. and Wheatley, Vincent (2018). Magnetohydrodynamic drag force measurements in an expansion tube. 9th AIAA Flow Control Conference 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-3755

Magnetohydrodynamic drag force measurements in an expansion tube

2018

Conference Publication

Expansion Tube Magnetohydrodynamic Experiments with Argon Test Gas

Gildfind, David E., Smith, Daniel, Lewis, Steven W., Kelly, Rory, James, Christopher M., Wei, Han and McIntyre, Timothy (2018). Expansion Tube Magnetohydrodynamic Experiments with Argon Test Gas. 2018 Flow Control Conference, Atlanta, Georgia, 25-29 June 2018. Reston, Virginia: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-3754

Expansion Tube Magnetohydrodynamic Experiments with Argon Test Gas

2018

Conference Publication

Rapid prototyping in instrumented hypervelocity testing

Eldridge, R., James, C.M., Apirana, S. and Morgan, R.G. (2018). Rapid prototyping in instrumented hypervelocity testing. 18th Australian Space Research Conference, Gold Coast, QLD, Australia, 24-26 September 2018.

Rapid prototyping in instrumented hypervelocity testing

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

2018

Conference Publication

Experimental study of saturn entry radiation with higher amount of diluent in an expansion tube

Liu, Yu, James, Christopher M., Morgan, Richard G. and McIntyre, Timothy J. (2018). Experimental study of saturn entry radiation with higher amount of diluent in an expansion tube. 12th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2018, Atlanta, GA United States, 25 - 29 June 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-4070

Experimental study of saturn entry radiation with higher amount of diluent in an expansion tube

2018

Conference Publication

Flow characterization and modeling of the X2 and X3 expansion tubes

Gildfind, David E., Jacobs, Peter A., Gollan, Rowan J., Toniato, Pierpaolo, McIntyre, Timothy J., Andrianatos, Andreas, James, Christopher M. and Morgan, Richard G. (2018). Flow characterization and modeling of the X2 and X3 expansion tubes. VKI Lecture Series STO-AVT-235 on Flow Characterization and Modeling of Hypersonic Wind Tunnels, Brussels, Belgium, 3-5 December 2018.

Flow characterization and modeling of the X2 and X3 expansion tubes

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

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