THERE are many instances in aeroplane design where the structures contain tension cables. If the structure is a “pure frame,” any error in the “truing up” will not occasion any additional forces in the various members; the only effect will be a slight distortion from its correct configuration. If, however, the structure is redundant, it is necessary that these cables be cut (or adjusted as the case may be) to their exact length; if not, the two joints to be connected will have to be distorted, thus causing the structure to become strained before any external loading has been applied. Such a structure is said to be “self-strained.” The forces in the various members, of course, depend upon the extent of the straining between the two joints concerned.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Self-Straining in Aeroplane Structures


    Untertitel :

    An Explanation of a Matter that is Frequently Found Puzzling by Students


    Beteiligte:
    Fox, James (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1933-12-01


    Format / Umfang :

    14 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    German aeroplane structures

    Engineering Index Backfile | 1942


    German aeroplane structures

    Engineering Index Backfile | 1942


    German aeroplane structures

    Engineering Index Backfile | 1942


    Fatigue in Aeroplane Structures

    Nissen, O. | Emerald Group Publishing | 1940


    AEROPLANE CONTROL SYSTEM, AEROPLANE AND AEROPLANE CONTROL METHOD

    YAMASAKI KOICHI | Europäisches Patentamt | 2015

    Freier Zugriff