A Nomad aileron was modified by the addition of strain gauges and associated wiring, to permit its use in loads-measurement trials. This modification rendered the aileron non-standard, so a flight flutter trial was conducted to verify the aeroelastic stability of the loads aircraft when fitted with this aileron. This report describes the flight flutter trial and presents the results.


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    Titel :

    Flight Flutter Test of a Nomad N24A Aircraft Fitted with One Modified Aileron


    Beteiligte:
    P. A. Farrell (Autor:in) / S. A. Dunn (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    37 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Vibration Test on a Nomad N24A Aircraft Fitted with One Modified Aileron

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    Falkner, Victor Montague / Jones, William Neville Prichard / Scruton, C. | TIBKAT | 1936


    Flutter experiments on a model wing fitted with a dead centre aileron control

    Falkner, Victor Montague ;Jones, William Neville Prichard ;Scruton, C. | SLUB | 1936


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    Scheubel, F.N. | Engineering Index Backfile | 1926