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Professor Anand Veeraragavan
Professor

Anand Veeraragavan

Email: 
Phone: 
+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

21 - 40 of 111 works

2021

Journal Article

Hypersonic shock impingement on a heated flat plate at Mach 7 flight enthalpy

Chang, Eric Won Keun, Chan, Wilson Y. K., McIntyre, Timothy J. and Veeraragavan, Ananthanarayanan (2021). Hypersonic shock impingement on a heated flat plate at Mach 7 flight enthalpy. Journal of Fluid Mechanics, 908 R1. doi: 10.1017/jfm.2020.877

Hypersonic shock impingement on a heated flat plate at Mach 7 flight enthalpy

2021

Journal Article

Spectral filtering of sub-bandgap radiation using all-dielectric gratings for thermophotovoltaic applications

Gupta, Murikipudi V. N. Surendra, Ameen, Elikkottil, Unnikrishnakurup, Sreedhar, Balasubramaniam, Krishnan, Veeraragavan, Ananthanarayanan and Pesala, Bala (2021). Spectral filtering of sub-bandgap radiation using all-dielectric gratings for thermophotovoltaic applications. Journal of Photonics for Energy, 11 (1), 015501-015501. doi: 10.1117/1.jpe.11.015501

Spectral filtering of sub-bandgap radiation using all-dielectric gratings for thermophotovoltaic applications

2020

Conference Publication

Supercritical Ethylene Gas Model for use in Internal Flow Paths

Trudgian, Matthew, Landsberg, Will and Veeraragavan, Anand (2020). Supercritical Ethylene Gas Model for use in Internal Flow Paths. 22nd Australasian Fluid Mechanics Conference AFMC2020, Brisbane, Australia, 7-10 December 2020. Brisbane, Australia: The University of Queensland. doi: 10.14264/05cef11

Supercritical Ethylene Gas Model for use in Internal Flow Paths

2020

Conference Publication

Dividing and Conquering: Supersonic Combustion of Ethylene with Varied Tandem Cavities

Hack, Flynn, Mecklem, Sarah, Landsberg, Will and Veeraragavan, Ananthanarayanan (2020). Dividing and Conquering: Supersonic Combustion of Ethylene with Varied Tandem Cavities. 22nd Australasian Fluid Mechanics Conference AFMC2020, Brisbane, QLD Australia, 7-10 December 2020. Brisbane, QLD Australia: The University of Queensland. doi: 10.14264/a1f4632

Dividing and Conquering: Supersonic Combustion of Ethylene with Varied Tandem Cavities

2020

Journal Article

Experimental scramjet combustion modes of hydrocarbon mixtures at Mach 8 flight conditions

Landsberg, Will O., Vanyai, Tristan, McIntyre, Timothy J. and Veeraragavan, Ananthanarayanan (2020). Experimental scramjet combustion modes of hydrocarbon mixtures at Mach 8 flight conditions. AIAA Journal, 58 (12), 1-6. doi: 10.2514/1.j059856

Experimental scramjet combustion modes of hydrocarbon mixtures at Mach 8 flight conditions

2020

Journal Article

Performance analysis and validation of an explicit local time-stepping algorithm for complex hypersonic flows

Damm, Kyle A., Landsberg, Will O., Mecklem, Sarah and Veeraragavan, Ananthanarayanan (2020). Performance analysis and validation of an explicit local time-stepping algorithm for complex hypersonic flows. Aerospace Science and Technology, 107 106321, 1-11. doi: 10.1016/j.ast.2020.106321

Performance analysis and validation of an explicit local time-stepping algorithm for complex hypersonic flows

2020

Journal Article

Dual/scram-mode combustion limits of ethylene and surrogate endothermically-cracked hydrocarbon fuels at Mach 8 equivalent high-enthalpy conditions

Landsberg, Will O., Vanyai, Tristan, McIntyre, Timothy J. and Veeraragavan, Ananthanarayanan (2020). Dual/scram-mode combustion limits of ethylene and surrogate endothermically-cracked hydrocarbon fuels at Mach 8 equivalent high-enthalpy conditions. Proceedings of the Combustion Institute, 38 (3), 3835-3843. doi: 10.1016/j.proci.2020.07.003

Dual/scram-mode combustion limits of ethylene and surrogate endothermically-cracked hydrocarbon fuels at Mach 8 equivalent high-enthalpy conditions

2020

Journal Article

Electrically-heated flat plate testing in a free-piston driven shock tunnel

Chang, Eric Won Keun, Chan, Wilson Y.K., Hopkins, Keill J., McIntyre, Timothy J. and Veeraragavan, Ananthanarayanan (2020). Electrically-heated flat plate testing in a free-piston driven shock tunnel. Aerospace Science and Technology, 103 105856, 105856. doi: 10.1016/j.ast.2020.105856

Electrically-heated flat plate testing in a free-piston driven shock tunnel

2020

Journal Article

Experimental investigation of inclining the upstream wall of a scramjet cavity

Trudgian, Matthew A., Landsberg, Will O. and Veeraragavan, Ananthanarayanan (2020). Experimental investigation of inclining the upstream wall of a scramjet cavity. Aerospace Science and Technology, 99 105767, 105767. doi: 10.1016/j.ast.2020.105767

Experimental investigation of inclining the upstream wall of a scramjet cavity

2020

Conference Publication

LES Simulation of Sound Generated by a Cylinder Wake and its Interaction with Shock Waves

Kaur, Ramandeep, Wheatley, Vincent, Veeraragavan, Anand and Doolan, Con (2020). LES Simulation of Sound Generated by a Cylinder Wake and its Interaction with Shock Waves. 22nd Australasian Fluid Mechanics Conference AFMC2020, Brisbane, QLD Australia, 7-10 December 2020. Brisbane, QLD Australia: The University of Queensland. doi: 10.14264/9760dbe

LES Simulation of Sound Generated by a Cylinder Wake and its Interaction with Shock Waves

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

Inclining and aerodynamically contouring a scramjet cavity's upstream wall

Landsberg, Will O. and Veeraragavan, Ananthanarayanan (2019). Inclining and aerodynamically contouring a scramjet cavity's upstream wall. Aerospace Science and Technology, 95 105490, 105490. doi: 10.1016/j.ast.2019.105490

Inclining and aerodynamically contouring a scramjet cavity's upstream wall

2019

Journal Article

Off-design performance of the supercritical carbon dioxide recompression Brayton cycle with NDDCT cooling for concentrating solar power

Duniam, Sam and Veeraragavan, Ananthanarayanan (2019). Off-design performance of the supercritical carbon dioxide recompression Brayton cycle with NDDCT cooling for concentrating solar power. Energy, 187 115992, 115992. doi: 10.1016/j.energy.2019.115992

Off-design performance of the supercritical carbon dioxide recompression Brayton cycle with NDDCT cooling for concentrating solar power

2019

Journal Article

Computational investigations on convective flow and heat transfer of turbulent supercritical CO2 cooled in large inclined tubes

Wang, Jianyong, Li, Jishun, Gurgenci, Hal, Veeraragavan, Ananthanarayanan, Kang, Xin and Hooman, Kamel (2019). Computational investigations on convective flow and heat transfer of turbulent supercritical CO2 cooled in large inclined tubes. Applied Thermal Engineering, 159 113922, 113922. doi: 10.1016/j.applthermaleng.2019.113922

Computational investigations on convective flow and heat transfer of turbulent supercritical CO2 cooled in large inclined tubes

2019

Journal Article

Fundamental scramjet combustion experiments using hydrocarbon fuel

Vanyai, Tristan, Grieve, Sam, Street, Oliver, Denman, Zachary, McIntyre, Timothy, Veeraragavan, Ananthanarayanan, Wheatley, Vincent and Smart, Michael (2019). Fundamental scramjet combustion experiments using hydrocarbon fuel. Journal of Propulsion and Power, 35 (5), 953-963. doi: 10.2514/1.B37472

Fundamental scramjet combustion experiments using hydrocarbon fuel

2019

Journal Article

A computationally derived heat transfer correlation for in-tube cooling turbulent supercritical CO2

Wang, Jianyong, Guan, Zhiqiang, Gurgenci, Hal, Veeraragavan, Ananthanarayanan, Kang, Xin and Hooman, Kamel (2019). A computationally derived heat transfer correlation for in-tube cooling turbulent supercritical CO2. International Journal of Thermal Sciences, 138, 190-205. doi: 10.1016/j.ijthermalsci.2018.12.045

A computationally derived heat transfer correlation for in-tube cooling turbulent supercritical CO2

2019

Conference Publication

Hypersonic shock impingement on a heated surface in the T4 free-piston driven shock tunnel

Chang, Eric W. K. , Chan, Wilson Y.K., McIntyre, Timothy J. and Veeraragavan, Ananthanarayanan (2019). Hypersonic shock impingement on a heated surface in the T4 free-piston driven shock tunnel. 32nd International Symposium on Shockwaves, Singapore, 14 - 19 July 2019. Piscataway, NJ, United States: IEEE.

Hypersonic shock impingement on a heated surface in the T4 free-piston driven shock tunnel

2019

Journal Article

Cavity flameholding in an optical axisymmetric scramjet in Mach 4.5 flows

Liu, Qili, Baccarella, Damiano, Landsberg, Will, Veeraragavan, Ananthanarayanan and Lee, Tonghun (2019). Cavity flameholding in an optical axisymmetric scramjet in Mach 4.5 flows. Proceedings of the Combustion Institute, 37 (3), 3733-3740. doi: 10.1016/j.proci.2018.08.037

Cavity flameholding in an optical axisymmetric scramjet in Mach 4.5 flows

2018

Journal Article

Numerical study on cooling heat transfer of turbulent supercritical CO2 in large horizontal tubes

Wang, Jianyong, Guan, Zhiqiang, Gurgenci, Hal, Veeraragavan, Ananthanarayanan, Kang, Xin, Sun, Yubiao and Hooman, Kamel (2018). Numerical study on cooling heat transfer of turbulent supercritical CO2 in large horizontal tubes. International Journal of Heat and Mass Transfer, 126 (B), 1002-1019. doi: 10.1016/j.ijheatmasstransfer.2018.06.070

Numerical study on cooling heat transfer of turbulent supercritical CO2 in large horizontal tubes

2018

Journal Article

Enhanced supersonic combustion targeting combustor length reduction in a Mach 12 scramjet

Landsberg, Will O., Wheatley, Vincent, Smart, Michael K. and Veeraragavan, Ananthanarayanan (2018). Enhanced supersonic combustion targeting combustor length reduction in a Mach 12 scramjet. AIAA Journal, 56 (10), 1-6. doi: 10.2514/1.j057417

Enhanced supersonic combustion targeting combustor length reduction in a Mach 12 scramjet

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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