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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    Titel :

    Dynamic Strength of Airplane Parts


    Weitere Titelangaben:

    Dynamische Festigkeit von Flugzeug-Konstruktionsteilen


    Beteiligte:
    Brenner, P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1928


    Format / Umfang :

    6 pages


    Anmerkungen:

    24 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Deutsch


    Schlagwörter :


    Dynamic Strength of Airplane Parts

    Brenner, P. | Engineering Index Backfile | 1929


    Dynamic breaking tests of airplane parts

    Hertel, H. | Engineering Index Backfile | 1933


    Dynamic destructive tests on airplane parts

    Hertel, H. | Engineering Index Backfile | 1931


    Plywood airplane parts

    Engineering Index Backfile | 1928


    Airplane parts and maintenance

    Wead, F.W. | Engineering Index Backfile | 1931