[Reports] / Amer.inst.of aeronautics and astronautics. N 89-0274 : implicit flux-vector splitting scheme for the computation of viscous hypersonic flow : Rep. presented at 27th aerospace sciences meet., Jan.9-12, 1989, Reno(Nv) / D.Hanel,R.Schwane, 1989. - 8 p. - Текст : непосредственный.