The purpose of this treatise is, first of all, the determination of the effect of variously loaded spars on one another, since the neglect of this effect would present an economically very unfavorable computation method. The system of spars and cross-bars alone (whether solid or built-up) does not matter at first, the original assumption being that the spars are rigidly braced by the cross-bars.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Computation of cantilever airplane wings


    Beteiligte:
    Thalau, K (Autor:in)

    Erscheinungsdatum :

    01.07.1925


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Computation of cantilever airplane wings

    Thalau, I. | Engineering Index Backfile | 1925


    Slotted airplane wings

    Engineering Index Backfile | 1921



    Airplane without wings

    WITMER WARNER H | Europäisches Patentamt | 2019

    Freier Zugriff

    Semi-cantilever wings

    Pasqualini, C. / Biro, D. | Engineering Index Backfile | 1935