Helicopter Active Flow Control Tests in the 14x22 Subsonic Wind
Helicopter active flow control tests in the 14X22 subsonic wind tunnel. Photos include preparation of the model before testing and the control room where testing is monitored and data collected
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Details
NASA ID
LRC-2013-00316
Date Created
June 3, 2013
Center
LRC
Media Type
image
Photographer
David Bowman
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