Impact damage resistance and residual strength of laminated composite transport aircraft fuselage structure was studied experimentally. Techniques to quantify impact damage discretely and non-discretely are described. Experimental techniques to three-dimensionally map matrix damage and determine the sublaminate structure are illustrated. Impact damage was also quantified non-discretely, using characteristics of flexural wave propagation Strain distributions in compressively loaded impact damaged laminates were experimentally measured.


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    Title :

    Experimental investigations into composite fuselage impact damage resistance and post-impact compression behavior


    Additional title:

    Experimentelle Untersuchungen bezüglich der Widerstandsfähigkeit gegen Stoßschäden von Flugzeugzellen aus Verbundwerkstoff und Kompressionsverhalten nach dem Stoß


    Contributors:
    Dost, E.F. (author) / Finn, S.R. (author) / Stevens, J.J. (author) / Lin, K.Y. (author) / Fitch, C.E. (author)


    Publication date :

    1992


    Size :

    14 Seiten, 12 Bilder, 10 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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