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NASA AFRC2017-0037-01, Armstrong flight research center

NASA AFRC2017-0037-01, Armstrong flight research center

 
 
description

Summary

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.

date_range

Date

17/02/2017
place

Location

AFRC
create

Source

NASA
copyright

Copyright info

Public Domain Dedication (CC0)