To Aerodynamic Design of Wings with Span Variable Profile in Incompressible Flow
| Authors: Pastukhov A.I., Galemin Ye.K. | Published: 02.09.2014 |
| Published in issue: #4(45)/2001 | |
| Category: Simulation of Processes | |
| Keywords: | |
A vortex model is studied in which the attached vortexes are distributed continuously along the wing surface, but the free ones come off its end. Vortex intensity in a wing section is obtained from the system of impenetrability equations formulated for points of this section.
