[Reports] / Amer.inst.of aeronautics and astronautics. N 89-0020 : interactive boundary-layer procedure for oscillating airfoils including transition effects : Paper presented at 27 aerospace sci.meeting, Jan.9-12, 1989, Reno(Nv) / T.Cebeci,L.W.Carr,H.M.jang, 1989. - 7 p. - Текст : непосредственный.