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Showing 1 to 1 of 1 for “"Velocity Isosurface"”.
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Influence of aspect ratio on dynamic stall of a finite wing
… through a series of three-component velocity measurements across different spanwise locations. The results revealed that the dynamic stall vortex originates with flow separation at the leading edge of the root section of the wing, displacing the shear-layer vorticity from the wing …