3-D shock wave-turbulent boundary layer interactions generated by a single fin / D. D. Knight, C. C. Horstman, G. S. Settles, 1993. - 23 p. - Текст : непосредственный.
[Reports] / Amer.inst.of aeronautics and astronautics. N 89-0082 : experimental study of shock wave/vortex interaction : Rep. presented at 27th Aerospace sciences meet., Jan.9-12, 1989, Reno(Nv) / O.M.Metwally,G.S.Settles,C.C.Horstman, 1989. - 12 p. - Текст : непосредственный.
Knight D. Supersonic turbulent flow past a 3-D swept compression corner at mach 3 : Papers presented at AIAA 26th aerospace sci.meet., Jan. 11-14, 1988, Reno(Nv). Pt. 2, 1988. - 17 p. - Текст : непосредственный.