The medium around the aircraft in hand is taken to be an ideal incompressible fluid, the aircraft’s surfaces are assumed impermeable. The flow is potential everywhere outside the aircraft and its vortex wake. The vortex wake represents a thin vortex sheet, i.e., a surface with a jump of the tangential component of the velocity field. The flow separation lines are taken to be the sharp edges of the aircraft’s surface.
Aerodynamic Loads on Aircraft Encountering Vortex Wakes of Other Aircraft
Foundations Engineering Mechanics
2009-06-13
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Lift Coefficient , Wind Flow , Vortex Wake , Aerodynamic Load , Rough Terrain Mathematics , Computational Mathematics and Numerical Analysis , Aerospace Technology and Astronautics , Classical and Continuum Physics , Engineering Fluid Dynamics , Numerical Analysis , Automotive Engineering , Engineering
British Library Conference Proceedings | 2010
|NTRS | 1970
|Vortex wakes of conventional aircraft
TIBKAT | 1975
|Vortex Wakes of large aircraft
TIBKAT | 1974
|Vortex Wakes of Conventional Aircraft
NTIS | 1975
|