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Dr Chris James
Dr

Chris James

Email: 
Phone: 
+61 7 336 53783

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

123 works between 2012 and 2026

1 - 20 of 123 works

Featured

2025

Journal Article

Expansion tube capabilities for studying boost-glide re-entry conditions

Lin, Yuhui, Wallington, James J., James, Christopher M., Bui, Thien, van den Herik, Toby J., Chang, Eric Won Keun and Hermann, Tobias A. (2025). Expansion tube capabilities for studying boost-glide re-entry conditions. CEAS Space Journal, 17 (4) 108087, 699-720. doi: 10.1007/s12567-025-00606-x

Expansion tube capabilities for studying boost-glide re-entry conditions

Featured

2025

Journal Article

Emission spectroscopy and surface temperature analysis from Hayabusa2 sample return observation

Liu, Yu, Thompson, Matthew, Apirana, Steven F. T., Morgan, Richard G. and James, Christopher M. (2025). Emission spectroscopy and surface temperature analysis from Hayabusa2 sample return observation. Acta Astronautica, 229, 498-511. doi: 10.1016/j.actaastro.2025.01.037

Emission spectroscopy and surface temperature analysis from Hayabusa2 sample return observation

Featured

2025

Journal Article

An intensified ultra-high-speed optical emission spectroscopy system for hypersonic impulse test facilities

Lu, Nathan H., Mcintyre, Timothy J., Jacobs, Carolyn, Andrianatos, Andreas and James, Christopher (2025). An intensified ultra-high-speed optical emission spectroscopy system for hypersonic impulse test facilities. Experiments in Fluids, 66 (4) 66. doi: 10.1007/s00348-025-03999-x

An intensified ultra-high-speed optical emission spectroscopy system for hypersonic impulse test facilities

Featured

2024

Journal Article

Large-scale free-piston-driven multi-mode shock expansion tunnel

Stennett, Samuel, Gildfind, David, Andrianatos, Andreas, Morgan, Richard, Jacobs, Peter, James, Christopher, Toniato, Pierpaolo, Chan, Wilson and Silvester, Todd (2024). Large-scale free-piston-driven multi-mode shock expansion tunnel. Experiments in Fluids, 65 (2) 16. doi: 10.1007/s00348-023-03756-y

Large-scale free-piston-driven multi-mode shock expansion tunnel

Featured

2024

Conference Publication

Implementation of microwave interferometry for continuous shock speed measurement in shock and expansion tubes

Straede, Henry G. B., Jenkinson, Isaac, van den Herik, Toby J. and James, Christopher M. (2024). Implementation of microwave interferometry for continuous shock speed measurement in shock and expansion tubes. 2024 AIAA Science and Technology Forum and Exposition, Orlando, FL, United States, 8-12 January 2024. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2024-2569

Implementation of microwave interferometry for continuous shock speed measurement in shock and expansion tubes

Featured

2022

Journal Article

Electron number density measurements in a Saturn entry condition

Liu, Yu, James, Christopher M., Morgan, Richard G., Jacobs, Peter A., Gollan, Rowan and McIntyre, Timothy J. (2022). Electron number density measurements in a Saturn entry condition. AIAA Journal, 60 (3), 1303-1315. doi: 10.2514/1.j060560

Electron number density measurements in a Saturn entry condition

Featured

2021

Journal Article

Experimental and computational fluid dynamics study of Hayabusa reentry peak heating

Fahy, Elise J., Buttsworth, David R., Gollan, Rowan J., Jacobs, Peter A., Morgan, Richard G. and James, Christopher M. (2021). Experimental and computational fluid dynamics study of Hayabusa reentry peak heating. Journal of Spacecraft and Rockets, 58 (6), 1833-1846. doi: 10.2514/1.a34863

Experimental and computational fluid dynamics study of Hayabusa reentry peak heating

Featured

2020

Journal Article

Experimentally Simulating Giant Planet Entry in an Expansion Tube

James, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W. and McIntyre, Timothy J. (2020). Experimentally Simulating Giant Planet Entry in an Expansion Tube. Journal of Spacecraft and Rockets, 57 (4), 1-16. doi: 10.2514/1.a34457

Experimentally Simulating Giant Planet Entry in an Expansion Tube

Featured

2019

Journal Article

Simulating gas giant atmospheric entry using helium and neon test gas substitutions

James, Christopher M., Gildfind, David E., Morgan, Richard G., Lewis, Steven W. and McIntyre, Timothy J. (2019). Simulating gas giant atmospheric entry using helium and neon test gas substitutions. Journal of Spacecraft and Rockets, 56 (3), 725-743. doi: 10.2514/1.a34282

Simulating gas giant atmospheric entry using helium and neon test gas substitutions

Featured

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

2026

Conference Publication

System Design and Preliminary Analysis of the University of Queensland Spectroscopy Data from the OSIRIS-REx Re-Entry Observation Mission

James, Christopher M., Lock, Samuel G., Lu, Nathan, van den Herik, Toby J., Morgan, Richard G., Zander, Fabian and Birch, Byrenn (2026). System Design and Preliminary Analysis of the University of Queensland Spectroscopy Data from the OSIRIS-REx Re-Entry Observation Mission. Reston, Virginia: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2026-2943

System Design and Preliminary Analysis of the University of Queensland Spectroscopy Data from the OSIRIS-REx Re-Entry Observation Mission

2026

Conference Publication

Development of New X2 Expansion Tube Test Conditions to Facilitate Low Density Non-Equilibrium Testing at 4 to 6 km/s

James, Christopher M., Hodson, Jaiden, van den Herik, Toby, Liu, Yu, Lock, Samuel, Wechgelaer, Noah and Morgan, Richard G. (2026). Development of New X2 Expansion Tube Test Conditions to Facilitate Low Density Non-Equilibrium Testing at 4 to 6 km/s. Reston, Virginia: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2026-2266

Development of New X2 Expansion Tube Test Conditions to Facilitate Low Density Non-Equilibrium Testing at 4 to 6 km/s

2025

Conference Publication

Free-piston driver performance at high compression ratios in the X2 expansion tube

van den Herik, Toby J., Thompson, M. and James, C. (2025). Free-piston driver performance at high compression ratios in the X2 expansion tube. 34th International Symposium on Shock Waves (ISSW34), Daegu, South Korea, 16-21 July 2023. Singapore: Springer. doi: 10.1007/978-981-96-4771-2_40

Free-piston driver performance at high compression ratios in the X2 expansion tube

2025

Conference Publication

Experimental study of turbulence-chemistry interactions for a blunted wedge at high-enthalpy

Wallington, James, Ananthapadmanaban, Ramprakash, Gildfind, David, Veeraragavan, Ananthanarayanan, Mee, David and James, Christopher M. (2025). Experimental study of turbulence-chemistry interactions for a blunted wedge at high-enthalpy. AIAA AVIATION FORUM AND ASCEND 2025, Las Vegas, NV, United States, 21 - 25 July 2025. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2025-3433

Experimental study of turbulence-chemistry interactions for a blunted wedge at high-enthalpy

2025

Conference Publication

Heat flux measurements of ice giant entry flows using near and mid-wave infrared thermography

Uren, Matthew, Lock, Samuel, Liu, Yu, James, Christopher M. and Morgan, Richard G. (2025). Heat flux measurements of ice giant entry flows using near and mid-wave infrared thermography. 3rd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry (FAR), Arcachon, France, 18-22 May 2025.

Heat flux measurements of ice giant entry flows using near and mid-wave infrared thermography

2025

Journal Article

A Eulerian-compatible split-cell scheme for piston tracking in high-enthalpy wind tunnels

Renzulli, L., D'Ambrosio, D., van den Herik, T., James, C. M., Veeraragavan, A., Mee, D. J. and Scalo, C. (2025). A Eulerian-compatible split-cell scheme for piston tracking in high-enthalpy wind tunnels. Physics of Fluids, 37 (3) 036126, 1-13. doi: 10.1063/5.0255887

A Eulerian-compatible split-cell scheme for piston tracking in high-enthalpy wind tunnels

2025

Conference Publication

Vacuum ultraviolet and visible spectral measurements for simulated Saturn entry in the X2 expansion tube

Liu, Y., Lock, S., Morgan, R. G. and James, C. M. (2025). Vacuum ultraviolet and visible spectral measurements for simulated Saturn entry in the X2 expansion tube. 34th International Symposium on Shock Waves, ISSW34 2023, Daegu, South Korea, 16-21 July, 2023. Singapore: Springer Nature. doi: 10.1007/978-981-96-4771-2_26

Vacuum ultraviolet and visible spectral measurements for simulated Saturn entry in the X2 expansion tube

2025

Conference Publication

Preliminary results for CO2 recombination for low velocity, high density mars entry conditions

Singh, M. P., Liu, Y., James, C. M., Morgan, R. G., Temme, N. and McIntyre, T. J. (2025). Preliminary results for CO2 recombination for low velocity, high density mars entry conditions. 34th International Symposium on Shock Waves (ISSW34), Daegu, South Korea, 16-21 July 2023. Singapore: Springer. doi: 10.1007/978-981-96-4771-2_34

Preliminary results for CO2 recombination for low velocity, high density mars entry conditions

2024

Conference Publication

Preheated blunt nose wedge model for shock tunnel testing

Scott, Pieter and James, Christopher M. (2024). Preheated blunt nose wedge model for shock tunnel testing. 14th Ablation Workshop, Laurel, MD United States, 5-7 November 2024.

Preheated blunt nose wedge model for shock tunnel testing

2024

Conference Publication

Ultra-highspeed optical emission spectroscopy: benefits and difficulties

Lu, Nathan, James, Christopher M., Jacobs, Carolyn and McIntyre, Timothy (2024). Ultra-highspeed optical emission spectroscopy: benefits and difficulties. 10th International Workshop on Radiation of High Temperature Gases for Space Missions, Oxford, United Kingdom, 9-12 September 2024.

Ultra-highspeed optical emission spectroscopy: benefits and difficulties

Funding

Current funding

  • 2025 - 2028
    Investigation of Ablation Products in the Near Wake of a High-Speed Hypersonic Vehicle
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2025 - 2026
    Experimental Validation of the MMT Thermochemical Nonequilibrium Air Chemistry Model in the X2 Free-piston Driven Expansion Tube
    United States Asian Office of Aerospace Research and Development
    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

Past funding

  • 2024
    Radiation reconstruction for ExoMars capsule flowfield
    AEDS Sarl
    Open grant
  • 2024 - 2025
    Characterisation and Modelling of Ablative Material Performance (DSP Research Agreement)
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2022 - 2026
    Experimental study of non-equilibrium turbulence-chemistry interaction in external hypersonic flows
    United States Office of Naval Research
    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

Looking for a supervisor? Read our advice on how to choose 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 NASA's upcoming Dragonfly 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