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Computational aeroelastic analysis of a hovering W3 Sokol blade with gurney flap [PDF]

open access: yesJournal of Fluids and Structures, 2015
This paper demonstrates the potential effect of a gurney flap on the performance of the W3-Sokol rotor blade in hover. A rigid blade was first considered and the calculations were conducted at several thrust settings. The gurney flap was extended from 46%
Rene Steijl, G N Barakos
exaly   +2 more sources
Some of the next articles are maybe not open access.

Characterization of the low-noise drone propeller with serrated Gurney flap

Frontiers in Aerospace Engineering, 2022
Toshiyuki Nakata
exaly  

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