A six-degree-of-freedom, nonlinear dynamic derivative sensitivity study has been conducted on a fighter/bomber and an attack-type aircraft. The dynamic derivatives investigated in the study were C sub lq, C sub mq, C sub mp, C sub mr, C sub l beta, and C sub n beta. For the cross-coupling derivatives, C sub lq was shown to have the most significant effect on the level and 3-g turning flight motion, followed by C sub nq and C sub mp with the derivative C sub mr showing little to negligible effect in the same regime. For the acceleration derivatives, C sub l beta was shown to have a significant influence on the aircraft motion. The C sub n beta derivative had little effect on the simulated motion. The analysis also documents the configuration dependency of the cross-coupling derivatives and investigates the effects of nonlinear variations in the derivatives on the aircraft motion. (Author)


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    Titel :

    Aircraft Motion Sensitivity to Dynamic Stability Derivatives


    Beteiligte:
    T. F. Langham (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    140 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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