Paper presents fatigue problem that developed in empennage area of Navy A3D aircraft, ground and flight test programs undertaken, and results; five areas where acoustical fatigue occurred most frequently and type and size of material listed; effective solution to cracking problem found was addition of elastomer at point where cracks occurred; procedure whereby tests results may be incorporated with analytical analysis to produce curves for design analysis. (See also SAE -- Paper for meeting n 164A Apr 5-8 1960 23 p)


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    Title :

    Acoustically induced fatigue -- Cause, solution and design analysis


    Additional title:

    SAE -- J


    Contributors:


    Publication date :

    1960


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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