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  • AIRCRAFT DESIGN, TESTING AND PERFORMANCE  (1)
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  • AIRCRAFT DESIGN, TESTING AND PERFORMANCE  (1)
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    Publication Date: 2019-07-13
    Description: The objective of this study was to investigate bandwidth concepts for deriving rotorcraft handling-qualities criteria from data obtained in two simulator experiments conducted at the Aeromechanics Laboratory. The first experiment was an investigation of the effects of helicopter vertical-thrust-response characteristics on handling qualities; the second experiment investigated the effects of helicopter yaw-control-response characteristics. In both experiments, emphasis was on low-speed Nap-of-the-Earth (NOE) tasks.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AD-A160664 , NAS 1.26:176709 , NASA-CR-176709 , International Conference, Rotorcraft Basic Research, American Helicopter Society; Feb 19, 1985 - Feb 21, 1985; Research Triangle Park, NC; United States
    Format: application/pdf
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