The fundamental static aeroelastic properties of a swept wing which has freedom to roll are studied. It is shown, using a simple example, that the divergence speed of a wing which can roll steadily is high or non-existent and consequently the rolling power of any aileron will vary almost linearly with dynamic pressure, and, in particular, remains finite at the fixed-root divergence speed. Inboard ailerons have higher reversal speeds than outboard ailerons when the wing is swept back but the opposite holds true when the wing is swept forward. Keywords: Aeroelasticity, Rolling power, Divergence, Great Britain. (SDW).


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    Titel :

    Wing Divergence and Rolling Power


    Beteiligte:
    L. T. Niblett (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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