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Heated Wall Supersonic Combustion Testing of Hydrocarbons in Axisymmetric Models in the T4/X3R Shock Tunnels at Mach 7-8 (2020–2023)

Grant type:
United States Asian Office of Aerospace Research and Development
Researchers:

  • Professor Anand Veeraragavan

    Professor
    School of Mechanical and Mining Engineering
    Faculty of Engineering, Architecture and Information Technology
    Professor
    Faculty of Engineering, Architecture and Information Technology
Funded by:
United States Department of Defense