“…The use of the VSL model made it possible to determine the influence of the second approximation effects in the laminar and turbulent flows around bodies with a large aspect ratio [81][82][83][84][85]. The following problems were solved within the framework of the VSL model: hypersonic airflow around bodies with a large aspect ratio with allowance for spatial transport of radiation and equilibrium reactions [86,87] with allowance for nonequilibrium thermal and chemical processes [81,88], supersonic nonuniform waketype flows around cones [89,90], and many others.…”