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
13.06.2009
27 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Flight Speed , Vertical Velocity , Axial Vortex , Vortex Core , Vortex Wake Automotive Engineering , Aerospace Technology and Astronautics , Engineering Fluid Dynamics , Mathematics , Numerical Analysis , Computational Mathematics and Numerical Analysis , Engineering , Classical and Continuum Physics
NTRS | 1970
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