When the streamlines in a flow turn with radius of curvature R, the

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Solved Assume that the streamlines for the wingtip vortices

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At the bottom of a loop in the vertical plane an airplane has a

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When the streamlines in a flow turn with radius of curvature R, the

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When the streamlines in a flow turn with radius of curvature R, the

Any ideas on how to lower the pressure differential in this turning vane? Ideally without adding extra aerodynamic components. : r /MechanicalEngineering

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