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    Title :

    Two stage damage tolerance evaluation of an aircraft fuselage panel with a circumferential crack and a broken stringer


    Contributors:

    Conference:

    54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference



    Publication date :

    2013-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Two Stage Damage Tolerance Evaluation of an Aircraft Fuselage Panel with a Circumferential Crack and a Broken Stringer

    Sayar, B.M. / Kayran, A. / American Institute of Aeronautics and Astronautics; American Society of Mechanical Engineers; American Society of Civil Engineers | British Library Conference Proceedings | 2013




    Influence of Bonded Crack Retarders on Damage Tolerance Performance of Fuselage Panel

    Zhang, Haiying / Dong, Dengke / Wei, Yulong et al. | Springer Verlag | 2019


    Aspects of Damage Tolerance of Aircraft Fuselage Structures

    Huber, K. / Pempe, A. / Zerbst, U. et al. | British Library Conference Proceedings | 2008