The Langley 1/8-scale V/STOL model tunnel was used to qualitatively determine the flow fields associated with semi-span close coupled canard wing and strake wing models. Small helium filled bubbles were injected upstream of the models to make the flow visible. Photographs were taken over the angle-of-attack ranges of -10 deg to 40 deg.
Flow visualization study of close-coupled canard wing and strake wing configuration
1975-03-03
Report
Keine Angabe
Englisch
Close-coupled canard-wing vortex interaction
AIAA | 1984
|Vortex-Wing Interaction of a Close-Coupled Canard Configuration
Online Contents | 1994
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