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; abstracts in Automotive Industries v 116 n 9 May 1 1957 p 126-7; Western Metals v 15 n 8 Aug 1957 p 51-4)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:

    Published in:

    Publication date :

    1957


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English