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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    Title :

    Reacting flight loads at forging temperatures


    Additional title:

    SAE -- Paper


    Contributors:
    Clay, E.O. (author)

    Conference:

    SAE Meeting ; 1961 Heat resisting



    Publication date :

    1961


    Size :

    4 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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