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Professor Anand Veeraragavan
Professor

Anand Veeraragavan

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+61 7 336 54069

Overview

Background

Prof. Anand Veeraragavan's research interests are in supersonic combustion of hydrocarbons, hypersonic aerothermodynamics, advanced optical diagnostics for hypersonic flows and microcombustion based portable power. He is the Co-Director for UQ's Centre for Hypersonics. Since 2021, he is an Associate Editor for the AIAA Journal of Spacecraft and Rockets, which is a Quartile 1 Journal in Aerospace Engineering (Scimago).

Prof. Anand Veeraragavan joined the School of Mechanical and Mining Engineering as a mechanical engineering lecturer in 2012. He was an Mid-Career Advance Queensland Research Fellow (2017-2020) awarded for conducting research in the project entitled

Supersonic Combustion of Hydrocarbon Fuels for High-Mach-Number Axisymmetric Scramjets

Anand graduated with a B.Tech in aerospace engineering from the Indian Institute of Technology Madras (IIT-Madras) in 2002. He obtained his MS (2006) and PhD (2009) degrees in aerospace engineering from the University of Maryland. His Doctoral research, which focused on understanding flame stabilization in microscale combustors, won the best thesis award in the Department of Aerospace Engineering at the University of Maryland.

After his PhD, he took up a research appointment as a postdoctoral research associate in the Device Research Lab at MIT where he worked on thermophotovoltaics and nanofluid based volumetric solar absorbers. He next joined GE Energy as a combustion technologist in the US. At GE, he worked primarily on designing the next generation, land based, heavy duty, gas turbine engine combustors focusing on cost, operability, reliability and emissions and also completed his lean Six Sigma Greenbelt certification at GE.

He is currently undertaking world-leading research in the field of hypersonics and supersonic combustion sponsored by Australian DST, U.S. Air Force Office of Scientific Research (AFOSR) and U.S. Asian Office of Aerospace Research and Development (AOARD). This includes leading the Australian effort in prestigious projects such as ground testing and simulations in support of the Boundary Layer Transition/Turbulence (BOLT II) flight test sponsored by the AFOSR.

His research interests include:

  • Supersonic combustion of hydrocarbon fuels
  • Hypersonic aerothermodynamics
  • Optical diagnostics: PLIF for supersonic combustion, FLDI for hypersonic aerothermodynamics, high-speed schlieren
  • Micro-combustion driven power systems
  • Solar thermal and solar photovoltaic technology development

Availability

Professor Anand Veeraragavan is:
Available for supervision
Media expert

Qualifications

  • Doctor of Philosophy, University of Maryland

Research interests

  • Anand Veeraragavan's research interests are:

    Hypersonics, High-speed Propulsion, Optical Diagnostics, Microcombustion, Solar Energy, Thermal Analysis/Modeling, Heat Exchangers, Modeling (CFD and Analytical), Energy Systems

Research impacts

A/Prof. Veeraragavan's research and service contributions have had several impacts in his fields.

1. Associate Editor of AIAA Journal of Spacecraft and Rockets: As the AE for this prestigious Quartile 1 journal, A/Prof. Veeraragavan provides leadership in the fields of hypersonics and space by processing articles reporting novel scientific outcomes. He draws upon his wide network of international experts to undertake impartial and critical reviews to uphold the high-standards that can be expected of JSR, along with his own expertise in these fields to provide a fair and fast review of submitted articles.

2. Presenter of the Australian hypersonics country report: For the last three editions in a row of the premier AIAA Space Planes and Hypersonics Systems and Technologies conference, A/Prof. Veeraragavan has been extended an invite by the organisers to present Australia's hypersonics activity to a world-wide audience. This engagement through his presentation allows for a quick synopsis of all of the key Australian hypersonics research to be assimilated and broadcast, allowing for specific follow-up contact to occur with relevant teams with collaborators around the world.

3. Panelist on VAIBHAV forum: A/Prof. Veeraragavan was invited in 2021 to participate in an initiative from the Indian Prime Minister's office called VAIBHAV. One of the thrusts of VAIBHAV was on hypersonics, specifically identifying key fundamental scientific topics that should be pursued in this field. A/Prof. Veeragavan featured as one of the main panelists along with eminent professors such as Prof. Lele (Stanford), Prof. Gaitonde (Ohio State), Prof. Gupta (U. Maryland) and participated actively in discussions and deliberations on the future of Indian hypersonics research and potential partnerships with overseas groups. A whitepaper arising from this panel discussion is under consideration with the Indian government for action.

4. Co-Secretary of Australasian Fluid Mechanics Conference: A/Prof. Veeragavan and colleagues from UQ and QUT jointly organised the 22nd Australasian Fluid Mechanics Conference in a hybrid mode overcoming the challenges of the COVID pandemic and providing a vital point of connection to fluid mechanicists both in Australia and overseas.

Works

Search Professor Anand Veeraragavan’s works on UQ eSpace

111 works between 2005 and 2025

101 - 111 of 111 works

2008

Conference Publication

2D analytical model investigating the effect of structural heat recirculation on the temperature profiles in a parallel plate reactor with a premixed laminar flame

Veeraragavan, Ananthanarayanan and Cadou, Christopher P. (2008). 2D analytical model investigating the effect of structural heat recirculation on the temperature profiles in a parallel plate reactor with a premixed laminar flame. ASME International Mechanical Engineering Congress and Exposition (IMECE2007), Seattle, WA, United States, 11-15 November 2007. New York, United States: American Society of Mechanical Engineers. doi: 10.1115/IMECE2007-43675

2D analytical model investigating the effect of structural heat recirculation on the temperature profiles in a parallel plate reactor with a premixed laminar flame

2007

Conference Publication

Simplified heat transfer analysis for flames in channels

Veeraragavan, A., Dellimore, K. and Cadou, C. (2007). Simplified heat transfer analysis for flames in channels. 39th AIAA Thermophysics Conference, Miami, FL, United States, 25 – 28 June 2007. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2007-3899

Simplified heat transfer analysis for flames in channels

2007

Conference Publication

Experimental burning velocity characteristics for premixed methane-air flames in a simulated microcombustor

Veeraragavan, Ananthanarayanan and Cadou, Chris (2007). Experimental burning velocity characteristics for premixed methane-air flames in a simulated microcombustor. 5th US Combustion Meeting 2007, California, USA, 25 – 28 March 2007. Combustion Institute.

Experimental burning velocity characteristics for premixed methane-air flames in a simulated microcombustor

2007

Conference Publication

Analytical solution for flame speed in micro channels

Veeraragavan, Ananthanarayanan and Cadou, Christopher (2007). Analytical solution for flame speed in micro channels. 5th US Combustion Meeting 2007, San Diego, CA, March 25, 2007-March 28, 2007. Combustion Institute.

Analytical solution for flame speed in micro channels

2007

Conference Publication

Experimental investigation of influence of heat recirculation on temperature distribution and burning velocity in a simulated micro-burner

Veeraragavan, A. and Cadou, C. (2007). Experimental investigation of influence of heat recirculation on temperature distribution and burning velocity in a simulated micro-burner. 45th AIAA Aerospace Sciences Meeting 2007, Reno, NV, United States, 8 – 11 January 2007. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2007-577

Experimental investigation of influence of heat recirculation on temperature distribution and burning velocity in a simulated micro-burner

2006

Conference Publication

Experimental and numerical investigation of flame stability and burning velocity in a micro burner using infrared diagnostics

Veeraragavan, A., Leach, T. and Cadou, C. (2006). Experimental and numerical investigation of flame stability and burning velocity in a micro burner using infrared diagnostics. 44th AIAA Aerospace Sciences Meeting 2006, Reno, NV, United States, 9 - 12 January 2007. Reston, VA, United States: American Institute of Aeronautics and Astronautics.

Experimental and numerical investigation of flame stability and burning velocity in a micro burner using infrared diagnostics

2006

Conference Publication

An integral approach to modeling sound propagation through a finite combustion zone

Veeraragavan, A., Pesala, Balasubrahmanyam and Sujith, R. I. (2006). An integral approach to modeling sound propagation through a finite combustion zone. 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, United States, 9 – 12 January 2006. Reston, VA, United States: The American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/6.2006-542

An integral approach to modeling sound propagation through a finite combustion zone

2006

Conference Publication

Modeling and simulation of the effects of axial diffusion on fuel-air mixing lengths in micro-power systems

Dellimore, K., Veeraragavan, A. and Cadou, C. (2006). Modeling and simulation of the effects of axial diffusion on fuel-air mixing lengths in micro-power systems. 44th AIAA Aerospace Sciences Meeting 2006, Reno, NV, United States, 9 – 12 January 2006. Reston, VA, United States: American Institute of Aeronautics and Astronautics.

Modeling and simulation of the effects of axial diffusion on fuel-air mixing lengths in micro-power systems

2005

Conference Publication

Infrared diagnostic technique for microscale combustors

Veeraragavan, Ananthanarayanan, Heatwole, Scott, Cadou, Christopher P. and Buckley, Steven G. (2005). Infrared diagnostic technique for microscale combustors. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States, 10 – 15 January 2005. Reston, VA, United States: AIAA. doi: 10.2514/6.2005-938

Infrared diagnostic technique for microscale combustors

2005

Conference Publication

Investigation of enhanced stability in micro-combustors

Leach, T., Veeraragavan, A. and Cadou, C. (2005). Investigation of enhanced stability in micro-combustors. Eastern States Section / Combustion Institute Fall Technical Meeting, Orlando, FL, United States, 13 – 16 November 2005. Pittsburgh, PA, United States: Combustion Institute.

Investigation of enhanced stability in micro-combustors

2005

Conference Publication

Near-Wall Measurements of Gas Temperature in Conventional-Scale and Micro-Scale Rockets

Cruz, Carlos A., Veeraragavan, Ananthanarayanan, Dellimore, Kiran, Cadou, Christopher and Marshall, Andre W. (2005). Near-Wall Measurements of Gas Temperature in Conventional-Scale and Micro-Scale Rockets. 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United States, 11 – 13 July 2005. Reston, VA, United States: AIAA.

Near-Wall Measurements of Gas Temperature in Conventional-Scale and Micro-Scale Rockets

Funding

Current funding

  • 2024 - 2025
    Ground testing and trajectory simulations of the BOLT 1b Hypersonic Boundary Layer Transition Flight Experiment
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2023 - 2026
    Expanding the scramjet operating envelope through oxygen enrichment
    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
  • 2023 - 2027
    3D Hypersonic Shock-Turbulent-Boundary-Layer Interactions
    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

  • 2021 - 2023
    Robust Adaptive Control of a Dual-Mode Scramjet with Targeted Uncertainty Quantification (USDOD University Consortium of Applied Hypersonics Project administered by the University of Michigan)
    University of Michigan
    Open grant
  • 2020 - 2023
    Heated Wall Supersonic Combustion Testing of Hydrocarbons in Axisymmetric Models in the T4/X3R Shock Tunnels at Mach 7-8
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2020 - 2024
    Advanced Ground Testing and Simulation of the Boundary Layer Transition (BOLT) Flight Experiment
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2019 - 2022
    Study of Non-Equilibrium Wakes Model
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2019
    Optical Equipment for Advanced Thermofluid Measurements
    UQ Major Equipment and Infrastructure
    Open grant
  • 2018 - 2024
    Hypersonic Science and Enabling Technologies - General Support
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2018 - 2022
    Examining Growth of Turbulence Over Heated Walls in Hypersonic Flows
    United States Air Force Office of Scientific Research
    Open grant
  • 2017 - 2021
    Supersonic Combustion of Hydrocarbon Fuels for High-Mach-Number Axisymmetric Scramjets
    Advance Queensland Research Fellowships
    Open grant
  • 2017 - 2019
    Experimental Studies of High-Speed Flows
    National University of Singapore Research Collaboration Agreement
    Open grant
  • 2017 - 2019
    Ethylene Fuelled Axisymmetric Scramjet Testing
    Commonwealth Defence Science and Technology Group
    Open grant
  • 2017 - 2018
    Enabling Hydrocarbons To Supersede Batteries For Portable Power Applications
    UQ Early Career Researcher
    Open grant
  • 2017 - 2019
    High power density motors incorporating advanced manufacturing methods (CRC - Project led by MagniX)
    Cooperative Research Centre Projects
    Open grant
  • 2016 - 2019
    Rapidly expanding non equilibrium hypersonic flow
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2016 - 2019
    Hydrocarbon fuel technology for hypersonic air breathing vehicles
    Cooperative Research Centre Projects
    Open grant
  • 2015 - 2017
    Mach 6-8 scramjet combustion experiments using hydrocarbon fuel
    United States Asian Office of Aerospace Research and Development
    Open grant
  • 2014
    True triaxial cell for advanced testing of porous media
    UQ Major Equipment and Infrastructure
    Open grant
  • 2013 - 2015
    The science of scramjet propulsion
    ARC Discovery Projects
    Open grant
  • 2012 - 2013
    Towards Microcombustion based Power Generation
    UQ New Staff Research Start-Up Fund
    Open grant

Supervision

Availability

Professor Anand Veeraragavan is:
Available for supervision

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

Available projects

  • Design of combustor for supersonic combustion of hydrocarbons in high Mach number scramjets

    This project directly relates to Dr. Veeraragavan's Advance Queensland mid-career Fellowship that will focus on developing scramjet technology capable of utilising longer chained hydrocarbons at Mach 7 - 8. I envisage there are at least two PhD projects to advance the state-of-the-art in the following:

    • Development of in-house CFD tools to be used for design space exploration of fundamental combustor concepts
    • Detailed investigation of cavity flame holders as 3-D artefacts, that has not received adequate attention for typical scramjet flow fields
    • Detailed investigation of thermal crackdown and ignition characteristics of kerosene like fuels under scramjet fuelling and injection conditions
    • Thermal management using composites/aniostropic materials in the combustors

    Interested students with a good chance at obtaining scholarships should get in touch. There may be a possibility to offer top-ups in excess of the scholarships along with required budget for travel to conferences and experimental/computational aspects of the project.

  • Shockwave Thermal Boundary Layer Interactions

    • Scramjet engine inlets and isolators experience shock trains
    • Shock trains will interact with the boundary layer that develops from the leading edge
    • Traditional studies do not consider a heated wall
    • These interactions can lead to scramjet engine unstart
    • The project will aim to characterise and control the negative impact of these interaction

Supervision history

Current supervision

Completed supervision

Media

Enquiries

Contact Professor Anand Veeraragavan directly for media enquiries about:

  • Combustion
  • Computational Fluid Dynamics
  • Concentrating Solar Energy
  • Heat Transfer
  • Hypersonics
  • Microcombustion
  • Solar Energy
  • Supersonic Combustion
  • System Integration
  • Thermal Power Cycles
  • Thermophotovoltaics

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