Aerodynamic Step Input Response of Electro-Active Membrane Wings

Barbu, Ioan-Alexandru; Kat, Roeland de; Ganapathisubramani, Bharathram

doi:10.2514/6.2017-0056

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2021

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“…In particular, they are shown to delay stall at large angles of attack due to the formation of a leading-edge vortex which is shed and convected downstream (Rojratsirikul et al, 2011). They can be used for flow control, for instance, active camber adjustment (Curet et al, 2014;Buoso and Palacios, 2016;Barbu et al, 2017). In this context, the role of the leading edge vortices is especially significant due to its relationship with the aerodynamic performance.…”

Section: Introductionmentioning

confidence: 99%