Impact of the formation angle on the drag of bio-inspired $\pmb \vee$-formations
Prasoon Suchandra, Shabnam Raayai-Ardakani

TL;DR
This study investigates how the formation angle in bio-inspired V-formation affects the flow field and drag reduction of fixed-wing aircraft or quad-rotors, revealing optimal angles for energy efficiency.
Contribution
It provides detailed flow analysis and quantifies drag reduction effects at various formation angles using particle image velocimetry, serving as a baseline for future wake interaction studies.
Findings
Maximum drag reduction (~80%) occurs for interior members at the tightest formation.
Drag reduction is observed for all members at formation angles around 50°.
Beyond 50°, only the leading member shows significant drag reduction.
Abstract
Bio-inspired flight formation is a well known technique for energy saving among groups of fixed-wing aircraft, and as of recently, for groups of quad-rotors. Here, we study the effect of the formation angle on the performance of each of the members of a 5-member -formation in terms of the flow field, and drag force. We employ axisymmetric cylinders, which are non-lifting in solo condition to reduce/eliminate the effect of the lift (lateral force) on the group performance, and use time-resolved, multi-illumination, consecutive-overlapping particle image velocimetry (PIV) to capture the velocity field around and in-between the members. Over a range of -formation angles, we see various degree of drag reduction, with the highest drag reduction () for the interior members of the tightest formation (formation with the smallest -angle and…
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