Research at North American Aviation in connection with design of Mach 3 fighter to find means to shield and insulate caps of wing support frames and wing carry-through members enclosing 2 J-93 engines; tensile properties at temperature of best high strength materials which include H-11 steels and nickel-cobalt alloys; problems involved of designing major load carrying portion of aircraft to ultra high temperatures; limited forms in which these metals can be produced; examples. (see also SAE -- J v 69 n 12 Dec 1961 p 64-5)


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    Titel :

    Reacting flight loads at forging temperatures


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Clay, E.O. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Heat resisting



    Erscheinungsdatum :

    1961


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Reacting Flight Loads at Forging Temperatures

    Clay, Eugene O. | SAE Technical Papers | 1961


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