Public domain
AFRC2017-0037-01
From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.
About this work
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.
NASA Image and Video Library’s own descriptionCredit lineAFRC2017-0037-01. NASA/AFRC, 2017-02-17. Public domain. ID: AFRC2017-0037-01.
