varies along the wingspan, and the loss in vortex strength is shed as a vortexsheet all along the trailing edge, rather than as a single trail at the wing-tips
to the wing develops along the whole wingspan because it is shed as a vortex-sheet from the trailing edge, rather than just as a single vortex from the
highly-swept wing leading-edge separation still occurs but instead creates a vortexsheet that rolls up above the wing producing spanwise flow beneath. Flow not
is forced to detach, curl and roll-up in the form of a vortexsheet. Later, the vortexsheet detaches from the feeding jet and propagates freely downstream
Zhukovsky and generally viewed as his successor. In 1913, they had created a vortex-sheet theory of aircraft propellers. In 1916, Vetchinkin and Zhukovsky created
vortex Vortex in axisymmetric stagnation point flows Jan Burgers Burgers vortexsheet Strained shear layer Jan Burgers Couette flow Laminar flow between two
Morgan (November 1974). "The interaction of sound with a semiinfinite vortexsheet". Quarterly Journal of Mechanics and Applied Mathematics. 27 (4): 465–487
approach), the drag force results from three natural phenomena: shock waves, vortexsheet, and viscosity. When the airplane produces lift, another drag component
relatively thin shear layer called a vortexsheet. The wingtip flow leaving the wing creates a tip vortex. As the main vortexsheet passes downstream from the trailing
vortex filament from the blade tips (and often the root), or a continuous vortexsheet from the blades' trailing edges. Lagrangian particle vortex methods can
local flow speed perturbation, which will be developed downstream to a vortexsheet. As a result, plasma actuators can behave as vortex generators. The difference