6th Applied Aerodynamics Conference 1988
DOI: 10.2514/6.1988-2582
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A comparative study of differing vortex structures arising in unsteady separated flows

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Cited by 7 publications
(9 citation statements)
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“…A great deal of information regarding unsteady aerodynamics has been gained through research at the University of Colorado [13][14][15][16][17][18][19]. Wind tunnel tests have been conducted for pitching and oscillating wings in constant fre estream velocity.…”
Section: Discussionmentioning
confidence: 99%
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“…A great deal of information regarding unsteady aerodynamics has been gained through research at the University of Colorado [13][14][15][16][17][18][19]. Wind tunnel tests have been conducted for pitching and oscillating wings in constant fre estream velocity.…”
Section: Discussionmentioning
confidence: 99%
“…This seems reasonable, because the flow would be characterized by deep stall and the boundary layer would be separated throughout the rotation cycle. Reatt achment of the boundary layer has also been shown to be a necessary condition for the generation of a cohesive vortex structure [13][14][15][16][17][18][19]. AOA variations in the post-stall regime, however, did result in weak, diffuse vortex formations, and additional lift compared with static values was observed.…”
Section: Tower Wake Effectsmentioning
confidence: 99%
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“…The formation of discrete, cohesive vortex structures may be considered part of the unsteady -__ separated flow development process. The formation of dynamic stall vortices has been seen in wind _ tunnel tests fbr pitching or oscillating airfoils [10][11][12][13][14][15][16][17][18][19]. Although the blades on this particular wind turbine do not pitch or oscillate, yawing of the rotor disk with respect to the wind, sudden wind gusts, or passage through the wake of a cylindrical tower may produce geometrically similar effects.…”
Section: Introductionmentioning
confidence: 99%