A wake vortex transport model has been developed which includes the effects of wind and wind
;
shear, buoyancy, mutual and self-induction, ground plane interaction, viscous decay, finite core
;
and Crow instability effects. Photographic and ground-wind vortex tracks obtained from DC-6, B-
;
747, B-707, and CV-880 aircraft flybys are compared with predicted vortex tracks computed using meteorological
;
and aircraft data as inputs to the transport model. A parametric analysis of the effects
;
of the aircraft, fluid mechanic, and meteorological parameters shows the relative magnitude of each
;
transport mechanism. The study constitutes the first detailed comparison of vortex transport theory
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with experimental data.
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