New structural problems which result from flight of aircraft under variable stress and elevated temperature conditions arising from aerodynamic heating; cumulative creep hypothesis suggested for use in analysis of life expectancy under variable stress and temperature conditions.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Life expectancy of aircraft under thermal flight conditions


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Gerard, G. (author)

    Published in:

    Publication date :

    1954


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English