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Comparing Numerical and Experimental Results for Drag Reduction by Active Flow Control Applied to a Generic Rotorcraft Fuselage

Comparing Numerical and Experimental Results for Drag Reduction by Active Flow Control Applied to a Generic Rotorcraft Fuselage

  • Presented at Forum 71
  • 17 pages
  • SKU # : 71-2015-059

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Comparing Numerical and Experimental Results for Drag Reduction by Active Flow Control Applied to a Generic Rotorcraft Fuselage

Authors / Details:
Caroline Lienard, Arnaud Le Pape, ONERA
Brian G. Allan, Norman W. Schaeffler, NASA Langley Research Center