THE paper suggests a new approach to the calculation of the bending strength of semi-monocoque (and possibly fully mono-coque) aircraft fuselage shells. The method described uses directly load-deflexion graphs obtained from laboratory compression tests on panels representative of the shell at the section under consideration, and is analogous to the calculation of the form factor for a solid beam section, which factor is dependent on the shape of the section and on the stress-strain relationship of the material of which the beam is made.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Bending of Fuselage Shells


    Untertitel :

    A New Approach, Based on Laboratory Compression Tests, that is Analogous to the Calculation of the Form Factor of a Solid Beam


    Beteiligte:
    Taylor, J.S. (Autor:in) / Harper, R.D.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1949-05-01


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Bending of fuselage shells

    Taylor, J.S. / Harper, R.D.M. | Engineering Index Backfile | 1949


    Fuselage shells

    Wingfield-Digby, F.J. | Engineering Index Backfile | 1944


    Integral Solutions for Fuselage Shells

    Zink, W. / Deutsche Gesellschaft fur Luft- und Raumfahrt / Confederation of European Aerospace Societies | British Library Conference Proceedings | 2001


    Frame for fuselage shells of an aircraft and fuselage shell

    AREVALO RODRIGUEZ ELENA / TORRES ESTEBAN ANTONIO | Europäisches Patentamt | 2022

    Freier Zugriff

    FRAME FOR FUSELAGE SHELLS OF AN AIRCRAFT AND FUSELAGE SHELL

    AREVALO RODRIGUEZ ELENA / TORRES ESTEBAN ANTONIO | Europäisches Patentamt | 2020

    Freier Zugriff