Title: Mach 10 experimental database of a three-dimensional scramjet inlet flow field
Subjects: Aerodynamics, Hypersonic, Air intakes, Airplanes, Computational fluid dynamics, Engine inlets, Flow distribution, Hypersonic Aerodynamics, Hypersonic speed, Inlet flow, Internal flow, Laminar boundary layer, Oblique shock waves, Pressure measurement, Ramjet engines, Scramjet engines, Shock wave interaction, Supersonic combustion ramjet engines, Three dimensional flow, Wind tunnel tests