2023
DOI: 10.1108/hff-01-2023-0046
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Design and implementation of spanwise lift and gust control via arrays of bio-inspired individually actuated pneumatic flaplets

Abstract: Purpose Covert feathers on avian wings can show dynamic pop-up behaviour in rapid succession as a reaction to turbulent gusts. The purpose of this paper is to understand the possible flow control mechanism induced during such dynamic motion cycles. A model aerofoil is designed with suction side spanwise control of rows of bio-inspired flaplets. Design/methodology/approach A NACA 0012 aerofoil is equipped with a spanwise row of eight flaplets at 80% chord, connected to pneumatic actuators and can be deployed … Show more

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(2 citation statements)
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“…The disturbance generation was realised with a symmetric NACA0012 wing (chord C1 = 30 cm) with four individually controlled pneumatically actuated flaplets, as previously developed in [25]. The pneumatic actuation was since updated from balloons to small pneumatic cartridge cylinders to overcome past repeatability concerns.…”
Section: Disturbance Generationmentioning
confidence: 99%
See 1 more Smart Citation
“…The disturbance generation was realised with a symmetric NACA0012 wing (chord C1 = 30 cm) with four individually controlled pneumatically actuated flaplets, as previously developed in [25]. The pneumatic actuation was since updated from balloons to small pneumatic cartridge cylinders to overcome past repeatability concerns.…”
Section: Disturbance Generationmentioning
confidence: 99%
“…Such distributed flaplets can help to control the distribution of circulation and drag along the span in a sensitive way. Such a wing was designed in our lab [25], and the individually controllable flaplets mimicked the pop-up feathers that birds have. This concept has been used as a disturbance generator in which the flaplets open and close to create a gust-like disturbance, and it will be used in such a way again here.…”
Section: Introductionmentioning
confidence: 99%