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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

107 works between 2005 and 2024

1 - 20 of 107 works

2024

Journal Article

Experimental verification of a modified cylindrical focused laser differential interferometer

Hopkins, Keill J., Ananthapadmanaban, Ramprakash, McIntyre, Timothy J., Mee, David J., Wheatley, Vincent and Veeraragavan, Ananthanarayanan (2024). Experimental verification of a modified cylindrical focused laser differential interferometer. Journal of Spacecraft and Rockets, 1-10. doi: 10.2514/1.a35842

Experimental verification of a modified cylindrical focused laser differential interferometer

2023

Journal Article

Examining Distributed Fueling Schemes Using Tandem Cavities in a Mach 8 Scramjet

Mecklem, Sarah A., Curran, Damian, Landsberg, Will O. and Veeraragavan, Ananthanarayanan (2023). Examining Distributed Fueling Schemes Using Tandem Cavities in a Mach 8 Scramjet. Journal of Spacecraft and Rockets, 61 (2), 1-11. doi: 10.2514/1.a35848

Examining Distributed Fueling Schemes Using Tandem Cavities in a Mach 8 Scramjet

2023

Conference Publication

Commissioning of a Supercritical Ethylene Fuel Injection System in the T4 Hypersonic Impulse Facility

Trudgian, Matthew A., Russell, Hugh, Vanyai, Tristan and Veeraragavan, Ananthanarayanan (2023). Commissioning of a Supercritical Ethylene Fuel Injection System in the T4 Hypersonic Impulse Facility. 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Bengaluru, India, 28 May - 1 June 2023. Reston, Virginia: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-3025

Commissioning of a Supercritical Ethylene Fuel Injection System in the T4 Hypersonic Impulse Facility

2023

Conference Publication

Measurements of Free stream Density Fluctuations in the T4 Stalker Tube

Ananthapadmanaban, Ramprakash, Veeraragavan, Ananthanarayanan, McIntyre, Timothy, Wheatley, Vincent and Mee, David (2023). Measurements of Free stream Density Fluctuations in the T4 Stalker Tube. 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Karnataka, India, 28 May - 1 June 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-3031

Measurements of Free stream Density Fluctuations in the T4 Stalker Tube

2023

Conference Publication

Trajectory-Based Conjugate Heat Transfer Simulation of the BoLT-II Flight Experiment

Damm, Kyle A., Gollan, Rowan and Veeraragavan, Anand (2023). Trajectory-Based Conjugate Heat Transfer Simulation of the BoLT-II Flight Experiment. AIAA SCITECH 2023 Forum, National Harbor, MD United States, 23-27 January 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0292

Trajectory-Based Conjugate Heat Transfer Simulation of the BoLT-II Flight Experiment

2023

Conference Publication

Heat transfer measurements of the BOLT II flight experiment model within the T4 reflected shock tunnel

Landsberg, Will O., Sandral, Jacob, Mee, David and Veeraragavan, Anand (2023). Heat transfer measurements of the BOLT II flight experiment model within the T4 reflected shock tunnel. AIAA SCITECH 2023 Forum, National Harbor, MD USA/Online, 23-27 January 2023. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0087

Heat transfer measurements of the BOLT II flight experiment model within the T4 reflected shock tunnel

2022

Conference Publication

Supersonic ethylene boundary layer combustion with a mutli-porthole injector array

Sandral, Jacob, Vanyai, Tristan, Veeraragavan, Anand and Wheatley, Vincent (2022). Supersonic ethylene boundary layer combustion with a mutli-porthole injector array. 23rd Australasian Fluid Mechanics Conference, Sydney, NSW, Australia, 4-8 December 2022. Perth, WA, Australia: Australasian Fluid Mechanics Society.

Supersonic ethylene boundary layer combustion with a mutli-porthole injector array

2022

Journal Article

Hypersonic shock impingement studies on a flat plate: flow separation of laminar boundary layers

Chang, Eric Won Keun, Chan, Wilson Y.K., McIntyre, Timothy J. and Veeraragavan, Ananthanarayanan (2022). Hypersonic shock impingement studies on a flat plate: flow separation of laminar boundary layers. Journal of Fluid Mechanics, 951 A19. doi: 10.1017/jfm.2022.827

Hypersonic shock impingement studies on a flat plate: flow separation of laminar boundary layers

2022

Journal Article

Numerical modeling and performance enhancement of micro combustor powered thermophotovoltaic systems using high contrast gratings

Surendra Gupta, M. V. N., Baig, Hasan, Ameen, E., Veeraragavan, Ananthanarayanan, Kumar Lakshmanan, Madan, Sujith, R. I. and Pesala, Bala (2022). Numerical modeling and performance enhancement of micro combustor powered thermophotovoltaic systems using high contrast gratings. Applied Thermal Engineering, 215 118935, 1-15. doi: 10.1016/j.applthermaleng.2022.118935

Numerical modeling and performance enhancement of micro combustor powered thermophotovoltaic systems using high contrast gratings

2022

Journal Article

Experimental flameholding performance of a scramjet cavity with an inclined front wall

Landsberg, Will O., Curran, Damian and Veeraragavan, Ananthanarayanan (2022). Experimental flameholding performance of a scramjet cavity with an inclined front wall. Aerospace Science and Technology, 126 107622, 1-10. doi: 10.1016/j.ast.2022.107622

Experimental flameholding performance of a scramjet cavity with an inclined front wall

2022

Journal Article

Combustion enhancement via tandem cavities within a Mach 8 scramjet combustor

Mecklem, Sarah A., Landsberg, Will O., Curran, Damian and Veeraragavan, Ananthanarayanan (2022). Combustion enhancement via tandem cavities within a Mach 8 scramjet combustor. Aerospace Science and Technology, 124 107551, 107551. doi: 10.1016/j.ast.2022.107551

Combustion enhancement via tandem cavities within a Mach 8 scramjet combustor

2021

Conference Publication

Hydrogen boundary layer combustion with multi-porthole injector arrays

Sandral, J., Vanyai, T., Veeraragavan, A. and Wheatley, V. (2021). Hydrogen boundary layer combustion with multi-porthole injector arrays. Australian Combustion Symposium 2021, Toowoomba, QLD Australia, 21-24 November 2021. Sydney, NSW Australia: Australia and New Zealand Combustion Institute.

Hydrogen boundary layer combustion with multi-porthole injector arrays

2021

Conference Publication

Influence of cavity depth on ignition and flameholding modes within a scramjet combustor

Landsberg, Will O., Curran, Damian and Veeraragavan, Anand (2021). Influence of cavity depth on ignition and flameholding modes within a scramjet combustor. ASCEND 2021, Las Vegas, NV United States, 15-17 November 2021. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-4163

Influence of cavity depth on ignition and flameholding modes within a scramjet combustor

2021

Conference Publication

Experimental design for investigating hydrocarbon injection in a hypersonic inlet

Street, Oliver, Landsberg, Will O., Vanyai, Tristan, Razzaqi, Sarah A. and Veeraragavan, Anand (2021). Experimental design for investigating hydrocarbon injection in a hypersonic inlet. ASCEND 2021, Las Vegas, NV United States, 15-17 November 2021. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-4120

Experimental design for investigating hydrocarbon injection in a hypersonic inlet

2021

Journal Article

Measurements and analysis of hypersonic tripped boundary layer turbulence

Hopkins, Keill J., Porat, Hadas, McIntyre, Timothy J., Wheatley, Vincent and Veeraragavan, Ananthanarayanan (2021). Measurements and analysis of hypersonic tripped boundary layer turbulence. Experiments in Fluids, 62 (8) 164. doi: 10.1007/s00348-021-03254-z

Measurements and analysis of hypersonic tripped boundary layer turbulence

2021

Journal Article

OH visualization of ethylene combustion modes in the exhaust of a fundamental, supersonic combustor

Vanyai, Tristan, Landsberg, Will O., McIntyre, Timothy J. and Veeraragavan, Ananthanarayanan (2021). OH visualization of ethylene combustion modes in the exhaust of a fundamental, supersonic combustor. Combustion and Flame, 226, 143-155. doi: 10.1016/j.combustflame.2020.11.037

OH visualization of ethylene combustion modes in the exhaust of a fundamental, supersonic combustor

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

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
  • 2018 - 2024
    Hypersonic Science and Enabling Technologies - General Support
    Commonwealth Defence Science and Technology Group
    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 - 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

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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

  • Doctor Philosophy

    Numerical investigation of advanced cavity flameholder designs for supersonic combustion of hydrocarbons for high Mach number scramjets

    Principal Advisor

  • Doctor Philosophy

    Injection of Supercritical and Near-Critical Fluids into Supersonic Crossflow

    Principal Advisor

    Other advisors: Emeritus Professor Michael Roberts, Dr Tristan Vanyai

  • Doctor Philosophy

    Examining the Growth of Hypersonic Boundary Layer Turbulence Over Heated Walls

    Principal Advisor

    Other advisors: Professor Vincent Wheatley, Professor Tim McIntyre

  • Doctor Philosophy

    Characterization of Boundary Layer Combustion via Distributed Injection

    Associate Advisor

    Other advisors: Dr Tristan Vanyai, Professor Vincent Wheatley

  • Doctor Philosophy

    Experimental Investigation of Turbulence Chemistry Interaction in High Enthalpy Flows

    Associate Advisor

    Other advisors: Dr David Gildfind, Dr Chris James

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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