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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.

Date
2016-11-22
Photographer / author
NASA/Carla Thomas
Collection
AFRC
Archive
NASA Image and Video Library
Type
photograph

Public domainsafest

Reason: a NASA work: not copyrighted in the United States.

Read from: NASA media usage guidelines: NASA material is not copyrighted in the US unless noted; no third-party credit or mark found.

Credit line

"AFRC2016-0356-08" (2016-11-22). NASA/AFRC/NASA/Carla Thomas. Public domain. https://images.nasa.gov/details/AFRC2016-0356-08

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