One-ninth-scale model hingeless and gimballed rotor-propellers were tested at an advance ratio of 0.7 in the Wright Brothers Wind Tunnel at MIT, in the presence of sinusoidal longitudinal and vertical gusts produced by a gust generator of novel design. The gimballed rotor was also subjected to sinusoidal collective and cyclic control inputs. Model test data in terms of blade inplane and out-of-plane bending, longitudinal and lateral gimbal motion, wing vertical and chordwise bending, and blade and wing torsion are presented and compared with theory.


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    Titel :

    A Study of Gust and Control Response of Model Rotor-Propellers in a Wind Tunnel Airstream


    Beteiligte:
    Ham, N. D. (Autor:in) / Bauer, P. H. (Autor:in) / Lawrence, T. H. (Autor:in) / Yasue, M. (Autor:in)

    Erscheinungsdatum :

    1975-08-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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