(NTF) National Transonic Facility Test 213-SFW Flow Control II,
(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. Image taken in building 1236, National Transonic Facility
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Details
NASA ID
LRC-2012-02442
Date Created
November 19, 2012
Center
LRC
Media Type
image
Photographer
George Homich
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