Data_for_3D_Density_Field_Reconstruction_from_Schlieren_and_Pressure

This dataset contains texture maps, flow field data, and aerodynamic pressure data on the surface of five different vehicle profiles under specific flight conditions, and is suitable for research in aerospace engineering, hydrodynamics, and related fields. The dataset covers the altitude range from 3000 to 4000 meters and the Mach number range from 2.0 to 2.75.