caa a22 4500 469100907 CHVBK 20180323133044.0 cr unu---uuuuu 170328e19920701xx s 000 0 eng 10.1007/BF01051338 doi (NATIONALLICENCE)springer-10.1007/BF01051338 Gorelov D. Omsk aut Integral equations in two-dimensional airfoil theory [Elektronische Daten] [D. Gorelov] A system of integral equations is obtained for the tangential components of the velocities on the upper and lower surfaces of a profile which does not have a parametric singularity connected with the thickness of the airfoil. An example of the solution of these equations by the discrete vortex method is given. This shows that they are highly effective for solving problems of flow over an airfoil of any, including arbitrarily small, thickness. Plenum Publishing Corporation, 1993 Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/4(1992-07-01), 586-589 0015-4628 27:4<586 1992 27 10697 https://doi.org/10.1007/BF01051338 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01051338 text/html Onlinezugriff via DOI NATIONALLICENCE 100 1- Gorelov D. Omsk aut NATIONALLICENCE 773 0- Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/4(1992-07-01), 586-589 0015-4628 27:4<586 1992 27 10697 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer