“…Many optical techniques such as schlieren, shadowgraph, holographic interferometry, particle image velocimetry (PIV), background oriented schlieren (BOS) [17][18][19][20], shadow-casting [21,22], laser induced fluorescence (LIF) [17,18] are extensively used in flow visualization in supersonic and hypersonic regimes in shock tunnels and wind tunnels. Among these, schlieren and shadowgraph schemes provide 2D projected qualitative images of the 3D domain, represented in intensity scale.…”