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Showing 1 to 1 of 1 for “"wind affect"”.
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A wind tunnel investigation of a wing-tip trailing vortex
A 3 'x2' subsonic wind tunnel has been constructed and calibrated. The flow in the wind tunnel accelerates 6.1 % along the test section due to boundary layer growth. The potential core flow at both the entrance and exit locations is strongly uniform. The mean velocity varies .4% across the entrance …