A thorough review of the existing impact test data and analysis methods was conducted and the results were used to identify a reliability prediction methodology for further development. The integrated residual strength/reliability method developed by Northrop Grumman under a Navy/Federal Aviation Administration sponsored program was selected and modified. The modification was primarily in reducing the number of empirical for the strength prediction. A structural damage tolerance evaluation was conducted using the modified model and the results compared to those obtained from the existing model.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Enhanced Reliability Prediction Methodology for Impact Damaged Composite Structures


    Beteiligte:
    H. P. Kan (Autor:in)

    Erscheinungsdatum :

    1998


    Format / Umfang :

    96 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    A Simple Progressive Failure Prediction Model for Impact-Damaged Composite Structures

    Russell, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008


    Compression Strength Prediction of Impact-Damaged Composite Sandwich Panels

    Ratcliffe, J. / Jackson, W. / Schaff, J. et al. | British Library Conference Proceedings | 2004


    Compression strength prediction of impact-damaged composite sandwich panels

    Ratcliffe, James / Jackson, Wade / Schaff, Jefferey | Tema Archiv | 2004


    Methodology for Testing Damaged Composite Helicopter Rotor Blades

    Vorotović, Goran / Bengin, Aleksandar / Mitrović, Časlav et al. | Springer Verlag | 2023