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  • 1985-1989  (1)
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    facet.materialart.
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    Preliminary study of a wing-tip vortex using laser velocimetry (1987)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Measurements have been made in the wake of a semi-span NACA 0015 airfoil with emphasis on the region of the wing tip vortex. The spanwise and streamwise velocity components were measured using a two-component laser Doppler velocimeter. The purpose of the study was to initiate the operation of a laser velocimeter system and to perform preliminary wake measurements in preparation for a more extensive study of the structure and near field development of a tip vortex.
    Keywords: AERODYNAMICS
    Type: NASA-TM-88343 , A-86207 , NAS 1.15:88343 , AVSCOM-TM-86-A-2
    Format: application/pdf
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