caa a22 4500 469100206 CHVBK 20180323133042.0 cr unu---uuuuu 170328e19920101xx s 000 0 eng 10.1007/BF01054164 doi (NATIONALLICENCE)springer-10.1007/BF01054164 Design of airfoil with flap simulated by a point vortex [Elektronische Daten] [N. Il'inskii, A. Potashev] The method of quasisolutions of inverse boundary-value problems (see [4]) is used to solve the problem of designing an airfoil with a flap, replaced by a fixed vortex, from given velocity distribution along the contour of the wing main part. Profiles are constructed and the effect of the flap (vortex) on the shape and aerodynamic properties of the mechanized wing is examined. Plenum Publishing Corporation, 1992 Il'inskii N. Kazan aut Potashev A. Kazan aut Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/1(1992-01-01), 1-6 0015-4628 27:1<1 1992 27 10697 https://doi.org/10.1007/BF01054164 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01054164 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Il'inskii N. Kazan aut NATIONALLICENCE 700 1- Potashev A. Kazan aut NATIONALLICENCE 773 0- Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/1(1992-01-01), 1-6 0015-4628 27:1<1 1992 27 10697 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer