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 inorder 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 vol. 72 no. 51, Dec. 22, 1928 pp. 24 figs)


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    Titel :

    Dynamic Strength of Airplane Parts


    Weitere Titelangaben:

    Dynamische festigkeit von flugzeug-konstruktionsteilen


    Beteiligte:
    Brenner, P. (Autor:in)


    Erscheinungsdatum :

    1929


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Dynamic Strength of Airplane Parts

    Brenner, P. | Engineering Index Backfile | 1928


    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