Results of investigation of metal shell-type fuselage for airplanes conducted by G. H. Martin Co. since 1927; no specific relation between body diameter and skin thickness; ratio of diaphragm spacing to stringer spacing; strength of skin alone and strength of stringers alone could be computed separately; effect of variation in cross-section shape; further studies for improvement of shell in relation to quantity production.


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    Titel :

    Recent improvements in airplane structures


    Weitere Titelangaben:

    Aviation Eng


    Beteiligte:
    Milburn, L.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1929


    Anmerkungen:

    2 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    RECENT AIRPLANE DESIGN AND PERFORMANCE IMPROVEMENTS

    MONTEITH, C N | SAE Technical Papers | 1922


    AIRPLANE - Experiences, benchmarks and improvements

    VASSBERG, JOHN / DAILEY, KATHLEEN | AIAA | 1990


    Airplane structures

    Engineering Index Backfile | 1938


    Airplane structures

    Niles, Alfred S. ;Newell, Joseph S. | SLUB | 1954


    Airplane structures

    Niles, Alfred S. ;Newell, Joseph S. | SLUB | 1950