2016
DOI: 10.2514/1.j054674
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Streamwise Oscillation of Airfoils into Reverse Flow

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Cited by 21 publications
(7 citation statements)
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“…In a cycle of the rotating rotor with variable-pitch motions, the oscillating airfoils often experience the advancing and retreating sides, characterized by the different placements of the airfoil geometry (Granlund et al, 2016). As the airfoil blunt leading edge confronts with the incoming flows, it is in forward mode, which has been investigated widely before.…”
Section: Tablementioning
confidence: 99%
“…In a cycle of the rotating rotor with variable-pitch motions, the oscillating airfoils often experience the advancing and retreating sides, characterized by the different placements of the airfoil geometry (Granlund et al, 2016). As the airfoil blunt leading edge confronts with the incoming flows, it is in forward mode, which has been investigated widely before.…”
Section: Tablementioning
confidence: 99%
“…More recent efforts have sought to expand the understanding of separated aerofoil flows to cases where the free-stream velocity is time varying (Choi, Colonius & Williams 2015;Granlund, Ol & Jones 2016;Kocher et al 2017;Kirk & Jones 2018). Of particular note, Dunne & McKeon (2015) considered the case of a NACA 0018 wing undergoing a simultaneous surging and pitching manoeuvre.…”
Section: Introductionmentioning
confidence: 99%
“…More recent efforts have sought to expand the understanding of separated aerofoil flows to cases where the free-stream velocity is time varying (Choi, Colonius & Williams 2015; Granlund, Ol & Jones 2016; Kocher et al. 2017; Kirk & Jones 2018).…”
Section: Introductionmentioning
confidence: 99%
“…Harbig, Sheridan & Thompson (2014) provided a detailed map of vortex stability over various advance ratios and aspect ratios for kinematics that included reverse flow, but the authors did not directly address changes in the two-dimensional (2-D) and three-dimensional (3-D) vortex dynamics. Granlund, Ol & Jones (2016) performed experiments that mirror the unsteady free stream experienced by a rotating wing in forward flight, but the authors did not investigate how their results would change in the presence of rotation.…”
Section: Introductionmentioning
confidence: 99%