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
Faculty of Engineering, Architecture and Information Technology
-
- Funded by:
- United States Department of Defense
