AFRC2017-0037-01
The Swept Wing Laminar Flow test article, integrated to the underside of a NASA F-15, will examine the effectiveness of different configurations of small dots, called distributed roughness elements, to extend smooth, laminar airflow over a wing’s depth, reducing friction drag.
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Details
NASA ID
AFRC2017-0037-01
Date Created
February 17, 2017
Center
AFRC
Media Type
image
Photographer
Ken Ulbrich
Location
AFRC
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