Explanation of why weight saving is so important and problems involved in keeping weight low without sacrificing anything of fundamental importance; effect of performance and military load on airplane size; foremost among newer materials are 75 ST aluminum alloy, SAE 4340 steel heat treated to 260,000 to 280,000 psi, and titanium; problem of engine selection.


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    Titel :

    Design of light-weight, high performance military aircraft


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1954



    Erscheinungsdatum :

    1954


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    DESIGN OF LIGHT-WEIGHT, HIGH-PERFORMANCE MILITARY AIRCRAFT

    HEINEMANN, E. H. | SAE Technical Papers | 1954




    Military possibilities of light aircraft

    Caldwell, C. | Engineering Index Backfile | 1941