caa a22 4500 469100524 CHVBK 20180323133043.0 cr unu---uuuuu 170328e19921101xx s 000 0 eng 10.1007/BF01051350 doi (NATIONALLICENCE)springer-10.1007/BF01051350 Design of an airfoil with a given velocity distribution near an interface [Elektronische Daten] [N. Il'inskii, M. Lotfullin, D. Maklakov, A. Potashev] Solutions for problems of profile design near a rigid wall or free surface are found as particular cases of the more general inverse problem of flow over an airfoil near an interface. The solution is based on a modification of the iteration method developed in [3, 4] for the direct problem of flow over a profile near an interface. In each step the apparatus of quasisolutions is employed. The calculations carried out demonstrate the efficiency of the method and reveal the effect of an interface, a rigid wall and a free surface on the geometric and aerodynamic characteristics of the profile. Plenum Publishing Corporation, 1993 Il'inskii N. Kazan' aut Lotfullin M. Kazan' aut Maklakov D. Kazan' aut Potashev A. Kazan' aut Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/6(1992-11-01), 766-771 0015-4628 27:6<766 1992 27 10697 https://doi.org/10.1007/BF01051350 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01051350 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Il'inskii N. Kazan' aut NATIONALLICENCE 700 1- Lotfullin M. Kazan' aut NATIONALLICENCE 700 1- Maklakov D. Kazan' aut NATIONALLICENCE 700 1- Potashev A. Kazan' aut NATIONALLICENCE 773 0- Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/6(1992-11-01), 766-771 0015-4628 27:6<766 1992 27 10697 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer