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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    Title :

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


    Contributors:
    P. A. Farrell (author) / S. A. Dunn (author)

    Publication date :

    1995


    Size :

    37 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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