[Reports] / Amer.inst.of aeronautics and astronautics. N 89-0357 : Experimental and numerical investigation of an oblique shock wave/turbulent boundary layer interaction with continuous suction : Rep. presented at 27th aerospace sciences meet.,Jan.9-12,1989/Reno(Nv) / D.Benhachmi,I.Greber,W.Hingst, 1989. - 13 p. . - Текст : непосредственный.
[Reports] / Amer.inst.of aeronautics and astronautics. 90-5240 : Experimental investigation of a single flush-mounted hypermixing nozzle : Rep.presented at the AIAA 2nd intern.aerospace planes conf. 29-31 Oct.29-31 Oct.1990 / D.Davis,W.Hingst,A.Porro, 1990. - 10 p. - Текст : непосредственный.