[Reports] / Amer.inst.of aeronautics and astronautics. N 89-0997 : Generation and control of separated vortices over a delta wing by means of leading edge : Rep. presented at the AIAA 2nd shear flow conf., Mar. 13-16,1989/Tempe(Az) / T.Karagounis,T.Maxworthy,G.R.Spedding, 1989. - 17 p. - Текст : непосредственный.