Thermal stresses set up in cellular wing structure when aircraft is subjected to change of speed or of altitude; for wings with little or no insulation maximum stress in wing is usually between 70 and 85% of value given by Young's modulus for webs X coefficient of expansion for skin X external temperature change; conclusion is that of metallic materials, combination of light alloy webs with steel skin is admirable for reducing thermal stresses.


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    Titel :

    Transient thermal stresses in wings


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Parkes, E.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1953


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Transient Thermal Stresses in Wings

    Parkes, E.W. | Emerald Group Publishing | 1953



    Thermal stresses near the roots of rectangular wings

    Pope, G. G. / Aeronautical Research Council | TIBKAT | 1961


    Aerodynamic stresses in airplane wings

    Huguenard, E. / Magnan, A. / Planiol, A. | Engineering Index Backfile | 1924