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(NTF) National Transonic Facility Test 213-SFW Flow Control II,
From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.
About this work
(NTF) National Transonic Facility Test 213-SFW Flow Control II, Fast-MAC Model: The fundamental Aerodynamics Subsonic Transonic-Modular Active Control (Fast-MAC) Model was tested for the 2nd time in the NTF. The objectives were to document the effects of Reynolds numbers on circulation control aerodynamics and to develop and open data set for CFD code validation.
NASA Image and Video Library’s own descriptionCredit line(NTF) National Transonic Facility Test 213-SFW Flow Control II,. NASA/LRC, 2012-11-19. Public domain. ID: LRC-2012-02447.
