“…The method resulting from this straightforward mixture of the DSD/SST concept and the compressible-flow SUPG method, which is now called compressible-flow ST SUPG method, was first tested in [83]. This was followed by computations for air intake of a jet engine with adjustable spool at supersonic speeds [84], aerodynamics of two high-speed trains in a tunnel [82], liquid propellant guns [85,86], and compressible-flow FSI [87,88]. Other progress included large-scale parallel computations [84,89], unified formulations of incompressible and compressible flows [76,90], and the development of stabilization parameters [78,[91][92][93].…”