AFRC2016-0356-08
Testing different configurations of distributed roughness elements on the Swept Wing Laminar Flow test article, seen suspended above, will allow NASA researchers to observe which distributions are most efficient in extending laminar flow over a supersonic aircraft’s wing.
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Details
NASA ID
AFRC2016-0356-08
Date Created
November 22, 2016
Center
AFRC
Media Type
image
Photographer
NASA/Carla Thomas
Location
AFRC
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