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
13.06.2009
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Rough Terrain , Lift Coefficient , Wind Flow , Aerodynamic Load , Vortex Wake Automotive Engineering , Aerospace Technology and Astronautics , Engineering Fluid Dynamics , Mathematics , Numerical Analysis , Computational Mathematics and Numerical Analysis , Engineering , Classical and Continuum Physics
British Library Conference Proceedings | 2010
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TIBKAT | 1974
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NTIS | 1975
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TIBKAT | 1965
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