[Reports] / Amer.inst.of aeronautics and astronautics. N 90-0149 : Numerical simulation of hypersonic oblique shock-wave/laminar boundary-layer interaction with shock induced combustion : Rep.presented at the AIAA 28th aerospace sciences meet.Jan.8-11,1990/Reno(Nv) / C.Chuck,S.Eberhardt, 1990. - 6,[5] p. - Текст : непосредственный.