Discussion of various factors which may give rise to alternating or fatigue stresses in airplane; main causes are aerodynamic and engine effects; parts most affected by engine vibration are engine bearers, radiator and fuel piping and controls; fundamentals of fatigue failure; examples; recommendations as to procedure in order to ensure that all aircraft members shall have sufficient strength against alternating stresses. Dynamic stresses and vibrations in airplanes; fatigue strength of alloys and metals used in airplane construction; examples from aviation practice illustrating failure by fatigue; methods of insuring dynamic strength in airplane construction. (see also translated abstract in Metallurgist (Supp. to Engineer), Apr. 26, 1929, pp. 52-53)


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    Title :

    Dynamic Strength of Airplane Parts


    Additional title:

    Dynamische Festigkeit von Flugzeug-Konstruktionsteilen


    Contributors:
    Brenner, P. (author)

    Published in:

    Publication date :

    1928


    Size :

    6 pages


    Remarks:

    24 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :


    Dynamic Strength of Airplane Parts

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