Publikationsdatum:
2019-06-28
Beschreibung:
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.
Schlagwort(e):
AERODYNAMICS
Materialart:
NASA-TM-88343
,
A-86207
,
NAS 1.15:88343
,
AVSCOM-TM-86-A-2
Format:
application/pdf
Permalink
