Citation:
V. N. Vetlutskii, T. V. Poplavskaya, “Compressible laminar boundary layer on a delta wing with attached shock wave”, Prikl. Mekh. Tekh. Fiz., 26:5 (1985), 23–29; J. Appl. Mech. Tech. Phys., 26:5 (1985), 624–629
This publication is cited in the following 3 articles:
V. N. Vetlutskii, T. V. Poplavskaya, “Computational analysis of a spatial compressed turbulent boundary layer on the upwind side of delta wings under supersonic flow”, J. Appl. Mech. Tech. Phys., 35:1 (1994), 69–74
V. N. Vetlutskii, T. V. Poplavskaya, “Numerical calculation of a three-dimensional laminar compressible boundary layer on profiled triangular wings with supersonic front edges”, J. Appl. Mech. Tech. Phys., 34:5 (1993), 677–682
V. N. Vetlutskii, T. V. Poplavskaya, “Calculation of a laminar boundary layer on the leeward side of a triangular plate with supersonic leading edges”, J. Appl. Mech. Tech. Phys., 30:1 (1989), 71–77