A free-piston-driven hypersonic test facility producing flight-representative high-enthalpy flows for re-entry, scramjet, planetary-entry, and high-speed aerothermodynamics research.
Identity
Name
University of Queensland T4 Shock Tunnel
Region
OC
Type
research_center
Details
Description
A free-piston-driven hypersonic test facility producing flight-representative high-enthalpy flows for re-entry, scramjet, planetary-entry, and high-speed aerothermodynamics research.