Skip to menu Skip to content Skip to footer
Dr Tristan Vanyai
Dr

Tristan Vanyai

Email: 
Phone: 
+61 7 336 51287

Overview

Background

Dr Tristan Vanyai's research interests are in the fields of hypersonic propulsion, aerodynamics, combustion visualisation and laser diagnostics, using both experimental and numerical techniques.

Dr Vanyai received his Doctor of Philosophy from The University of Queensland in 2018, after completing a Bachelor of Aerospace Engineering (First Class Honours) and Bachelor of Science double degree at Monash University in 2012.

His research focuses on fundamentals of hypersonic propulsion through the scramjet cycle. Robust combustion within low intake compression scramjets is a key technology enabler for hypersonic accelerator vehicles, and can be achieved through utilising techniques such as thermal compression. Dr Vanyai is examining the improvements to scramjet combustion due to thermal compression through experiments in the T4 Stalker Tube facility using advanced optical techniques and comparison with results from numerical simulations.

Availability

Dr Tristan Vanyai is:
Available for supervision
Media expert

Qualifications

  • Bachelor of Science, Monash University
  • Bachelor (Honours), Monash University
  • Doctor of Philosophy, The University of Queensland

Research interests

  • Hypersonic Propulsion and Aerodynamics

  • Combustion Visualisation

  • Laser Diagnostics

Works

Search Professor Tristan Vanyai’s works on UQ eSpace

30 works between 2014 and 2025

21 - 30 of 30 works

2020

Journal Article

Correction: Fundamental scramjet combustion experiments using hydrocarbon fuel (Journal of Propulsion and Power, (2019) 5, 5, (953-963), 10.2514/1.B37472)

Vanyai, Tristan, Grieve, Sam, Street, Oliver, Denman, Zachary, McIntyre, Timothy, Veeraragavan, Ananthanarayanan, Wheatley, Vincent and Smart, Michael (2020). Correction: Fundamental scramjet combustion experiments using hydrocarbon fuel (Journal of Propulsion and Power, (2019) 5, 5, (953-963), 10.2514/1.B37472). Journal of Propulsion and Power, 36 (6), AU5-AU5. doi: 10.2514/1.B37472.c1

Correction: Fundamental scramjet combustion experiments using hydrocarbon fuel (Journal of Propulsion and Power, (2019) 5, 5, (953-963), 10.2514/1.B37472)

2019

Journal Article

Thermal and mixing efficiency enhancement in nonuniform-compression scramjets

Bricalli, Mathew G., Brown, Laurie, Boyce, Russell R. and Vanyai, Tristan (2019). Thermal and mixing efficiency enhancement in nonuniform-compression scramjets. AIAA Journal, 57 (11), 4778-4791. doi: 10.2514/1.J057908

Thermal and mixing efficiency enhancement in nonuniform-compression scramjets

2018

Journal Article

Scramjet Performance with Nonuniform Flow and Swept Nozzles

Bricalli, Mathew G., Brown, Laurie, Boyce, Russell R., Gollan, Rowan, Vanyai, Tristan and Pudsey, Adrian S. (2018). Scramjet Performance with Nonuniform Flow and Swept Nozzles. AIAA Journal, 56 (10), 1-16. doi: 10.2514/1.j056963

Scramjet Performance with Nonuniform Flow and Swept Nozzles

2018

Other Outputs

Experimental Investigation of a 3D Thermal Compression Scramjet Using Advanced Optical Techniques

Vanyai, Tristan (2018). Experimental Investigation of a 3D Thermal Compression Scramjet Using Advanced Optical Techniques. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland. doi: 10.14264/uql.2018.247

Experimental Investigation of a 3D Thermal Compression Scramjet Using Advanced Optical Techniques

2018

Conference Publication

Fundamental scramjet combustion experiments using hydrocarbon fuel

Vanyai, Tristan, Grieve, Sam, Street, Oliver, Denman, Zachary, McIntyre, Timothy, Veeraragavan, Anand, Wheatley, Vincent and Smart, Michael (2018). Fundamental scramjet combustion experiments using hydrocarbon fuel. AIAA International Space Planes and Hypersonics Systems and Technologies Conference, AIAA SPACE Forum, Orlando, FL, United States, 17–19 September 2018. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2018-5201

Fundamental scramjet combustion experiments using hydrocarbon fuel

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

OH imaging in a non-uniform, hydrogen-fueled scramjet engine

Vanyai, Tristan, Brieschenk, Stefan and McIntyre, Timothy J (2017). OH imaging in a non-uniform, hydrogen-fueled scramjet engine. 11th Asia-Pacific Conference on Combustion, ASPACC 2017, Sydney, Australia, 10-14 December 2017. Sydney, Australia: Combustion Institute.

OH imaging in a non-uniform, hydrogen-fueled scramjet engine

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

2014

Conference Publication

Quasi-one-dimensional investigation of combustion processes on scramjet performance

Vanyai, Tristan, Bricalli, Mathew, Brieschenk, Stefan and Boyce, Russell R. (2014). Quasi-one-dimensional investigation of combustion processes on scramjet performance. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014, Atlanta, GA, United States, 16-20 June 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2014-2786

Quasi-one-dimensional investigation of combustion processes on scramjet performance

2014

Conference Publication

L1 augmentation configuration for a lateral/directional manoeuvre of a hypersonic glider in the presence of uncertainties

Banerjee, Sanchito, Vanyai, Tristan, Wang, Zhongjie, Baur, Bernhard and Holzapfel, Florian (2014). L1 augmentation configuration for a lateral/directional manoeuvre of a hypersonic glider in the presence of uncertainties. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014, Atlanta, GA, United States, 16-20 June 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2014-2533

L1 augmentation configuration for a lateral/directional manoeuvre of a hypersonic glider in the presence of uncertainties

Funding

Current funding

  • 2025 - 2027
    Effect of Magnetic Field Deflection on Magnetohydrodynamic Heat Shield
    ARC Discovery Projects
    Open grant
  • 2023 - 2025
    Investigating the Influence of Tailored Wall Temperature Profiling on Hypersonic Boundary Layer Transition
    United States Asian Office of Aerospace Research and Development
    Open grant

Past funding

  • 2019 - 2024
    Transpiration Cooling to Enable Sharp Leading Edge Technology
    University of Oxford
    Open grant

Supervision

Availability

Dr Tristan Vanyai is:
Available for supervision

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

Available projects

  • Thermal compression scramjet performance over an access-to-space trajectory

    Dr Tristan Vanyai has funding for a PHD project examining performance of fundamental scramjet engines. By encouraging non-uniformity in a scramjet flow path, local regions can become hot enough to ignite fuel-air mixtures in combustors that would otherwise have average, overall temperatures that are too low. This process has been shown numerically and experimentally to improve performance for hydrogen fuel at specific flight conditions, however we must examine whether an access-to-space vehicle’s performance is improved over the full hypersonic trajectory. In this project, a student will conduct numerical simulations and/or experiments with combustion visualisation to examine performance improvements over a baseline, uniform flow path.

    If you are interested in this topic, please contact t.vanyai@uq.edu.au

Supervision history

Current supervision

Completed supervision

Media

Enquiries

Contact Dr Tristan Vanyai directly for media enquiries about:

  • Aerospace Engineering
  • Laser Diagnostics
  • Scramjets
  • Supersonic Combustion

Need help?

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

communications@uq.edu.au