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Experimental/Numerical Evaluation Of Integral Trailing Edge Flaps For Helicopter Rotor Applications

Experimental/Numerical Evaluation Of Integral Trailing Edge Flaps For Helicopter Rotor Applications

  • Presented at Forum 56
  • 19 pages
  • SKU # : 56-00046

  • Your Price : $30.00

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Experimental/Numerical Evaluation Of Integral Trailing Edge Flaps For Helicopter Rotor Applications

Authors / Details: Ahmed A. Hassan, The Boeing Company; Friedrich K. Straub, The Boeing Company; Kevin W. Noonan, NASA Langley Research Center