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- W266070744 abstract "This chapter describes the influence of the aircraft wake on the downwind dispersal of ULV sprays. The behavior of spray droplets released into an aircraft wake will depend principally on the drop size and release position relative to the vortex flow field. As most agricultural aircraft have typical vortex flow velocities of up to 1–2 m s −1 , the motion of all drops smaller than 500 μm will be dominated by vortex flow. Estimates indicate that drops released from all positions along the wing will be accelerated toward the vortex core. As a result of the higher velocities near the wing tips, only those drops released close to the wing tip will actually get near to the vortex core. Actual drop penetration of the core does not occur for drops greater than a few microns, because of the centrifugal forces involved. Thus, drops tend to remain in an equilibrium position on the periphery of the core. The upper boundary of the spray cloud increased as it drifted until at 120 m it was just grazing the topmost sampling point." @default.
- W266070744 created "2016-06-24" @default.
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- W266070744 date "1980-01-01" @default.
- W266070744 modified "2023-09-27" @default.
- W266070744 title "The Influence of the Aircraft Wake on the Downwind Dispersal of ULV Sprays" @default.
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- W266070744 doi "https://doi.org/10.1016/b978-0-08-022425-1.50040-1" @default.
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