Time-averaged near-wake of a yawed cylinder
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The near-wake of a cylinder with yaw angles from 0° to 45° by 5° steps was investigated.

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Two distinct flow patterns with a transitional pattern were identified in the near-wake.

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The direction of the backflow approached to that of the streamwise with increasing yaw.

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The spanwise vortices shed nearly parallel to the cylinder axis.

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The magnitude of the flow unsteadiness was generally reduced with increasing yaw.

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