This paper discusses the observations and results from an experimental investigation of cross ply laminates used to construct major structural components of a small aircraft manufactured in Australia. The static and fatigue experimental results are compared with established models in composites analysis and with the available data in composite databases. An analysis was done to statistically quantify any deviation of actual properties from the calculated values and investigate the differences in designed and actual capacities/operational life of the components made using this laminates. Experimentally obtained properties of industrial grade material woven glass/epoxy laminates, has shown a reasonable agreement with the calculated properties of the laminate using laminate theory. The material also showed good fatigue properties and comparatively the fatigue data of this material are consistent with fatigue data of similar laminates available in composite databases.


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    Title :

    An experimental investigation of the properties of cross-ply laminate used for manufacturing of small aircraft components


    Additional title:

    Eine experimentelle Untersuchung der Eigenschaften von Cross-ply-Laminaten für die Herstellung von Komponenten für kleine Flugzeuge


    Contributors:


    Publication date :

    2006


    Size :

    7 Seiten, 14 Bilder, 4 Tabellen, 12 Quellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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