We are performing Direct Numerical Simulation (DNS) of supersonic zero-pressure gradient (ZPG) turbulent spatially-developing boundary layers at a Mach number of 2.5 and at the incompressible regime, as well.
The extensive information supplied by DNS is used to evaluate the compressibility effects on turbulent coherent structures via Two-Point Correlations (TPC) of flow fluctuations.
The data gathered from the DNS is converted into 3D virtual objects toachieve a more immersive glance. Virtual Reality and Augmented Reality is used for our Virtual Wind Tunnel and FlowVisXR in-house mobile application.