The medium in which the aircraft is traveling is an ideal incompressible fluid, the aircraft’s surfaces are assumed to be impermeable [78]. The flow is potential everywhere outside the aircraft and its vortex wake. The vortex wake represented a thin vortex sheet, i.e., a surface of discontinuity for the tangential component of the velocity field. The flow separation lines are taken to be sharp edges of the aircraft’s surfaces.
Vortex Wakes Behind Propeller-Driven Aircraft
Foundations Engineering Mechanics
2009-06-13
27 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Vertical Velocity , Vortex Core , Vortex Wake , Flight Speed , Axial Vortex Mathematics , Computational Mathematics and Numerical Analysis , Aerospace Technology and Astronautics , Classical and Continuum Physics , Engineering Fluid Dynamics , Numerical Analysis , Automotive Engineering , Engineering