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(NTF) National Transonic Facility Test 213-SFW Flow Control II,

George Homich2012-11-19

NASA

NASA

(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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  • Title: (NTF) National Transonic Facility Test 213-SFW Flow Control II,
  • Creator: George Homich
  • Date Created: 2012-11-19
  • Rights: LRC
  • Album: edrobin1

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