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Second Test Of A Helicopter Individual Blade Control System In The NASA ANES 40 By 80 Foot Wind Tunnel

Second Test Of A Helicopter Individual Blade Control System In The NASA ANES 40 By 80 Foot Wind Tunnel

  • 18 pages
  • SKU # : sm_1995_NE_19_13_Jacklin

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Second Test Of A Helicopter Individual Blade Control System In The NASA ANES 40 By 80 Foot Wind Tunnel

Authors / Details: Stephen A. Jacklin, NASA Ames Research Center; Achim Blaas, ZF Luftfahrttechnik, GmbH; Stephen M. Swanson, Sterling Software; Dietrich Teves, Eurocopter Deutschland, GmbH