The report presents data on (1) residual strength of aircraft panels containing Multiple-Site Damage (MSD) in lap splices, and (2) fatigue strength of panels subjected to cyclic pressure loading. The testing was conducted using the dedicated Aging Aircraft Test Facility previously built in the Foster-Miller laboratory. A previous report describes the work in the first phase involving the design and operation of the facility and the test data generated on residual strength of panels with longitudinal midday skin cracks.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Full-Scale Testing and Analysis of Curved Aircraft Fuselage Panels


    Contributors:
    G. Samavedam (author) / D. Hoadley (author) / D. Thomson (author)

    Publication date :

    1993


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    VIRTUAL TESTING OF AIRCRAFT FUSELAGE STIFFENED PANELS

    Linde, P. / Pleitner, J. / Rust, W. et al. | British Library Conference Proceedings | 2004


    Methodology for Testing Curved Fuselage Panels under Biaxial Loading Conditions

    Fleischer, T. / Schoenfeld, D. / International Committee on Aeronautical Fatigue | British Library Conference Proceedings | 1997


    AIRCRAFT FUSELAGE ASSEMBLY JIG AND METHOD FOR HANDLING AIRCRAFT FUSELAGE PANELS

    KASAHARA KENJI / SEGAWA SHUHEI | European Patent Office | 2017

    Free access

    Full-scale testing, inspection, and modeling of damaged hoeeyeomb sandwich composite fuselage panels

    Leonie, F.A. / Bakuckas, J.G. / Awerbuch, J. et al. | Tema Archive | 2009


    Full-Scale Testing and Analysis of Fuselage Structure

    Miller, M. / Gruber, M. L. / Wilkins, K. E. et al. | British Library Conference Proceedings | 1994