Problem at subsonic speeds; trend towards use of large single piece aircraft components; use of alloy steel; advantages of titanium alloys at temperature of 200 F; above 700 F, stainless steel and cobalt base alloys seem to be most promising; usable flight spectra of various materials discussed are shown graphically.


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    Title :

    Selection of aircraft construction materials


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:
    Shaw, S.L. (author)

    Conference:

    Society of Automotive Engineers -- Meeting ; 1954 Selection



    Publication date :

    1954


    Size :

    5 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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