Aircraft Wake Vortex Alleviation: An Experimental Approach
Omer El Matbagi
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Aircraft Wake Vortex Alleviation: An Experimental Approach

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Motivation behind the present investigation is the alleviation of the rolling moment induced on the following aircraft by means of a DSS¿s. Particle image velocimetry was used to characterize wing tip vortex structures as well as quantifying vortex meandering. DSS capabilities in modifying the span-wise wing load and further reduces the wake vortex hazard were carried out. PIV technique was used to measure the wake velocities down-stream of the aircraft half model. Results reveal a noticeable inboard shift of wing loading along with the direct interaction of the spoiler¿s wake and flap tip v...