Citation:
V. N. Vetlutskii, T. V. Poplavskaya, “Numerical calculation of a three-dimensional laminar compressible boundary layer on profiled triangular wings with supersonic front edges”, Prikl. Mekh. Tekh. Fiz., 34:5 (1993), 88–94; J. Appl. Mech. Tech. Phys., 34:5 (1993), 677–682