[Reports] / Amer.inst.of aeronautics and astronautics. N 89-0353 : Mach number dependence of flow separation induced by normal shock wave turbulen boundary layer interaction at a curved wall : Rep. presented at the 27th aerospace sciences meet.,Jan.9-12,1989/Reno(Nv) / P.Doerffer,U.Dallmann, 1989. - 9 p. - Текст : непосредственный.
Doerffer P. Spatial and temporal features of a separated flow field at a convex wall induced by normal shock wave turbulent boundary layer interaction : Paper presented at AIAA 21st fluid dynamics,plasma dynamics and lasers conf.,June 18-20,1990,Seattle,Wa. / P.Doerffer,U.Dallmann, 1990. - 11 p. - Текст : непосредственный.