University Consortium for Applied Hypersonics Seminar Series: Discrete Roughness Boundary-Layer Transition at Hypersonic Conditions
Boundary layer transition at hypersonic conditions is a critical design concern for all future high-speed missions and vehicles. As part of the vehicle design process, accurate methods are needed to predict transition behavior in flight, in order to correctly model the aerothermodynamic environments used to size a hypersonic vehicle’s thermal protections system. In almost every […]