THERMAL stresses in aircraft structures arise from the long established fact that most of the common engineering materials expand with increase of temperature. The subject has become a problem due to the fact that increases in aircraft performance arc resulting in much greater variations and rates of variation of temperature than have hitherto been experienced. One solution to the problem would be to use only materials which do not change their physical dimensions with temperatures. However, although such materials do exist, it is probably asking too much of the metallurgist to expect him to produce alloys possessing this property in addition to the many others demanded by the aircraft structural engineer.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Problem of Thermal Stresses in Aircraft Structures


    Untertitel :

    A Paper Presented at the Bristol Conference on Thermal Stress Organized by the Stress Analysis Group of the Institute of Physics on January 7, 1954, and Summarized in the Report of the Conference in the February issue


    Beteiligte:
    Loveless, E. (Autor:in) / Boswell, A.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1954-04-01


    Format / Umfang :

    3 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Problem of thermal stresses in aircraft structures

    Loveless, E. / Boswell, A.C. | Engineering Index Backfile | 1954


    Alleviation of thermal stresses in aircraft structures

    Capey, E. C. / Aeronautical Research Council | TIBKAT | 1965


    Thermal stresses in aircraft structures repaired with bonded patches

    Woerden, Henricus J.M. / Van Der Meijs, Ronaldus M. | Tema Archiv | 2004