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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Dynamic Strength of Airplane Parts


    Additional title:

    Dynamische festigkeit von flugzeug-konstruktionsteilen


    Contributors:
    Brenner, P. (author)


    Publication date :

    1929


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Dynamic breaking tests of airplane parts

    Hertel, H. | Engineering Index Backfile | 1933


    Dynamic destructive tests on airplane parts

    Hertel, H. | Engineering Index Backfile | 1931


    Finishing airplane parts

    Coyle, J.C. | Engineering Index Backfile | 1929


    Wood-plastic airplane parts

    Bates, C.L. | Engineering Index Backfile | 1942


    Phenolic fibre in airplane parts

    Stedman, G.E. | Engineering Index Backfile | 1945