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Numerical Investigation of Rotorcraft Fuselage Drag Reduction using Active Flow Control

Numerical Investigation of Rotorcraft Fuselage Drag Reduction using Active Flow Control

  • Presented at Forum 67
  • 24 pages
  • SKU # : 67-2011-000111

  • Your Price : $30.00

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Numerical Investigation of Rotorcraft Fuselage Drag Reduction using Active Flow Control

Authors / Details: Brian Allan, NASA Langley Research Center; Norman Schaeffler, NASA Langley Research Center