Problems resulting from increased temperature associated with high speed flight investigated at Lockheed research laboratory; means available for solving such problems for structures flying in intermediate hypersonic range; subject considered under three headings: aerodynamic heating, structural configurations for thermal flight, and production problems. (See also Soc Automotive Engrs -- Paper n 84 for meeting Apr 2-5 1957 42 p; Western Metals v 15 n 8 Aug 1957 p 51-4; Soc Automotive Engrs -- J v 65 n 9 Aug 1957 p 38-42)


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    Title :

    Problems in application of high strength steel alloys in design of supersonic aircraft


    Additional title:

    Automotive Industries


    Contributors:

    Published in:

    Automotive Industries ; 116 , n 9 ; p 126-127


    Publication date :

    1957


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English