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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.
Nothing Found.
Tags
afrc
armstrong flight research center
swept wing laminar flow
ken ulbrich
high resolution
experimental aircraft
nasa
Date
17/02/2017
Location
AFRC
Source
NASA
Link
Copyright info
Public Domain Dedication (CC0)