The effects of changes in aileron rigging between 2 deg up and 2 deg down on the stick forces were determined from wind-tunnel data for a finite-span wing model. These effects were investigated for ailerons deflecting equally in both directions and linearly with stick deflection. Data were analyzed for a Frise, a sealed internally balanced, and a beveled-trailing-edge aileron. The results of the analysis showed that only ailerons having linear hinge-moment characteristics are unaffected by changes in rigging and indicated that ailerons having decidedly nonlinear hinge-moment-coefficient curves, particularly for deflections near 0 deg, are very sensitive to changes in rigging.


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    Titel :

    Effect of Changes in Aileron Rigging on the Stick Forces of a High-Speed Fighter Airplane


    Beteiligte:
    Murray, Harry E. (Autor:in) / Warren, S Anne (Autor:in)

    Erscheinungsdatum :

    1944-05-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Effect of changes in aileron rigging on stick forces of high-speed fighter airplane

    Murray, H.E. / Warren, S.A. | Engineering Index Backfile | 1944





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