Oct 15 1941 n 8 p 26-31: Results of experiments conducted at New York University with Ken Royce 90 and Wright R-540-E 5-cyl radial engines; determination of turning moments, bending moments and stresses. Nov 15 n 10 p 32-3 and 45: Conclusion and application of results; tabu-later values for maximum positive and negative turning moments.


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    Titel :

    Bending moments in master rods of radial aircraft engines


    Weitere Titelangaben:

    Automotive Industries


    Beteiligte:
    Porter, L.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1941


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Bending moments in master rod of radial aircraft engine

    Taylor, C.F. | Engineering Index Backfile | 1932


    Bending Moments in the Master Rod of a Radial Aircraft Engine

    Taylor, C. F. | SAE Technical Papers | 1932


    Vibration of radial aircraft engines

    Bentley, G.P. | Engineering Index Backfile | 1939


    New data on bending moments in master connecting rod

    Taylor, C.F. | Engineering Index Backfile | 1933


    Fracture of glass rods in bending and under radial pressure

    Gurney, C. / Rowe, P. W. | TIBKAT | 1948