Public domain
Helicopter Active Flow Control Tests in the 14x22 Subsonic Wind
From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.
About this work
Helicopter active flow control tests in the 14X22 subsonic wind tunnel.
NASA Image and Video Library’s own descriptionSubjects
Credit lineHelicopter Active Flow Control Tests in the 14x22 Subsonic Wind. NASA/LRC, 2013-06-04. Public domain. ID: LRC-2013-00319.
