Skip to menu Skip to content Skip to footer
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

99 works between 2012 and 2024

1 - 20 of 99 works

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

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

2024

Conference Publication

HYPULSE Modelling using Quasi-0D Analytical Framework

Heffernan, Liam, James, Christopher M. and Jewell, Joseph S. (2024). HYPULSE Modelling using Quasi-0D Analytical Framework. Reston, Virginia: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.2024-4566

HYPULSE Modelling using Quasi-0D Analytical Framework

2023

Journal Article

Investigation of visible to near-infrared high-speed cameras for thermography in hypersonic testing

Alemany, Loïc G., James, Christopher M., Cullen, Timothy G. and Liu, Yu (2023). Investigation of visible to near-infrared high-speed cameras for thermography in hypersonic testing. Experiments in Fluids, 64 (12) 189, 1-16. doi: 10.1007/s00348-023-03731-7

Investigation of visible to near-infrared high-speed cameras for thermography in hypersonic testing

2023

Conference Publication

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

Singh, M., Liu, Y., James, C.M., Morgan, R.G., Temme, N. and McIntyre, T.J. (2023). Preliminary results for CO2 recombination for low velocity, high density mars aerocapture conditions. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023.

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

2023

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. (2023). Vacuum ultraviolet and visible spectral measurements for simulated saturn entry in the X2 expansion tube. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023.

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

2023

Conference Publication

Development of Microwave Sensor for Measurement of X2 Expansion Tube Shock Speeds

Jenkinson, Isaac, James, C.M. and Straede, H. (2023). Development of Microwave Sensor for Measurement of X2 Expansion Tube Shock Speeds. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023.

Development of Microwave Sensor for Measurement of X2 Expansion Tube Shock Speeds

2023

Conference Publication

High enthalpy free-piston driver conditions in the X2 expansion tube for ice giant planetary entry

van den Herik, T., Thompson, M. and James, C.M. (2023). High enthalpy free-piston driver conditions in the X2 expansion tube for ice giant planetary entry. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023.

High enthalpy free-piston driver conditions in the X2 expansion tube for ice giant planetary entry

2023

Conference Publication

Experimental VUV shock layer radiation measurements for 13 and 14 km/s high speed earth re-entry conditions

Lock, S., Liu, Y., Morgan, R., James, C. and McIntyre, T. (2023). Experimental VUV shock layer radiation measurements for 13 and 14 km/s high speed earth re-entry conditions. 34th International Symposium on Shock Waves, Daegu, South Korea, 16-21 July 2023.

Experimental VUV shock layer radiation measurements for 13 and 14 km/s high speed earth re-entry conditions

2023

Journal Article

Correction: Magnetohydrodynamic Experiments of Total Heat Flux Mitigation for Superorbital Earth Reentry

Lefevre, Alexis, Gildfind, David E., Gollan, Rowan J., Jacobs, Peter A. and James, Christopher M. (2023). Correction: Magnetohydrodynamic Experiments of Total Heat Flux Mitigation for Superorbital Earth Reentry. AIAA Journal, 61 (6), 1-1. doi: 10.2514/1.j061771.c1

Correction: Magnetohydrodynamic Experiments of Total Heat Flux Mitigation for Superorbital Earth Reentry

2023

Journal Article

Correction: Expansion Tube Experiments of Magnetohydrodynamic Aerobraking for Superorbital Reentry

Lefevre, Alexis, Gildfind, David E., Gollan, Rowan J., Jacobs, Peter A., McIntyre, Timothy J. and James, Christopher M. (2023). Correction: Expansion Tube Experiments of Magnetohydrodynamic Aerobraking for Superorbital Reentry. AIAA Journal, 61 (4), 1-1. doi: 10.2514/1.j060253.c1

Correction: Expansion Tube Experiments of Magnetohydrodynamic Aerobraking for Superorbital Reentry

2023

Conference Publication

Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in X3 Expansion Tunnel

Kennedy, Aaron, Penty Geraets, Rowland T., James, Christopher M., Thompson, Matthew, Morgan, Richard G., Austin, Joanna M., Zander, Fabian and McGilvray, Matthew (2023). Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in X3 Expansion Tunnel. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0271

Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in X3 Expansion Tunnel

2023

Journal Article

Correction: Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in the X3 Expansion Tunnel (American Institute of Aeronautics and Astronautics Inc, AIAA)

Kennedy, Aaron, Geraets, Rowland Penty, James, Christopher, Thompson, Matthew, Morgan, Richard, Austin, Joanna, Zander, Fabian and McGilvray, Matthew (2023). Correction: Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in the X3 Expansion Tunnel (American Institute of Aeronautics and Astronautics Inc, AIAA). AIAA SciTech Forum and Exposition, 2023. doi: 10.2514/6.2023-0271.c1

Correction: Measurements of Hypersonic Double Cone Flows with Shock Wave/Boundary Layer Interactions in the X3 Expansion Tunnel (American Institute of Aeronautics and Astronautics Inc, AIAA)

2022

Conference Publication

Testing a free flying model of the ESA IXV in the X2 expansion tube

Wallington, J.J. and James, C.M. (2022). Testing a free flying model of the ESA IXV in the X2 expansion tube. 23rd Australasian Fluid Mechanics Conference, Sydney, NSW Australia, 4-8 December 2022.

Testing a free flying model of the ESA IXV in the X2 expansion tube

2022

Conference Publication

University of Queensland near infrared spectroscopy of the Hayabusa2 re-entry

James, Christopher M., Liu, Yu, Thompson, Matthew and Apirana, Steven F. T. (2022). University of Queensland near infrared spectroscopy of the Hayabusa2 re-entry. AIAA AVIATION 2022 Forum, Chicago, IL USA, 27 June-1 July 2022. Reston, VA USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2022-3735

University of Queensland near infrared spectroscopy of the Hayabusa2 re-entry

2022

Conference Publication

Optimisation of super orbital earth re-entry conditions in an expansion tunnel

Curtis, Kieren, James, Christopher M., Lock, Sam, Lu, Nathan and Lewis, Steven W. (2022). Optimisation of super orbital earth re-entry conditions in an expansion tunnel. AIAA Aviation 2022 Forum, Chicago, IL United States, 27 June - 1 July 2022. Reston, Virginia: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2022-3420

Optimisation of super orbital earth re-entry conditions in an expansion tunnel

2022

Conference Publication

Ultrahigh-speed emission spectroscopy for flow analysis in laboratory environments

Lu, Nathan, Andrianatos, Andreas, James, Christopher M., Jacobs, Carolyn and McIntyre, Timothy (2022). Ultrahigh-speed emission spectroscopy for flow analysis in laboratory environments. AIAA Aviation 2022 Forum, Chicago, IL United States, 27 June - 1 July 2022. Reston, Virginia: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2022-3419

Ultrahigh-speed emission spectroscopy for flow analysis in laboratory environments

2022

Journal Article

Magnetohydrodynamic experiments of total heat flux mitigation for superorbital earth reentry

Lefevre, Alexis, Gildfind, David E., Gollan, Rowan J., Jacobs, Peter A. and James, Christopher M. (2022). Magnetohydrodynamic experiments of total heat flux mitigation for superorbital earth reentry. AIAA Journal, 60 (9), 1-14. doi: 10.2514/1.j061771

Magnetohydrodynamic experiments of total heat flux mitigation for superorbital earth reentry

2022

Journal Article

Coaxial Thermocouple Heat Flux Measurements in Heavily Ionized Flows with Magnetic Fields

Lefevre, Alexis, Gildfind, David E. and James, Christopher M. (2022). Coaxial Thermocouple Heat Flux Measurements in Heavily Ionized Flows with Magnetic Fields. Journal of Thermophysics and Heat Transfer, 36 (4), 1-7. doi: 10.2514/1.t6446

Coaxial Thermocouple Heat Flux Measurements in Heavily Ionized Flows with Magnetic Fields

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

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