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Acoustic Results From a Full-Scale Wind Tunnel Test Evaluating lndividual Blade Control

Acoustic Results From a Full-Scale Wind Tunnel Test Evaluating lndividual Blade Control

  • Presented at Forum 51
  • 20 pages
  • SKU # : 51_1_034

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Acoustic Results From a Full-Scale Wind Tunnel Test Evaluating lndividual Blade Control

Authors / Details: Stephen M. Swanson, Sterling Software, Inc.; Stephen A. Jacklin, NASA Ames Research Center; Achim Blaas, ZF Luftfahrttechnik, GmbH; Georg Niesl, Eurocopter Deutschland, GmbH; and Roland Kube, DLR, Institute of Flight Mechanics