STP174: Stress-Rupture Properties of Inconel 700 and Correlation on the Basis of Several Time-Temperature Parameters

    Manson, S. S.
    National Advisory Committee for Aeronautics, Lewis Flight Propulsion Laboratory, Cleveland, Ohio

    Succop, G.
    National Advisory Committee for Aeronautics, Lewis Flight Propulsion Laboratory, Cleveland, Ohio

    Pages: 7    Published: Jan 1956


    Abstract

    The primary purpose of the present investigation was to determine the properties of Inconel 700, which appears promising for use at temperatures in the region of 1600 F; a simultaneous objective was to check the validity of various time-temperature parameters proposed in the literature for correlating hightemperature stress-rupture data.


    Paper ID: STP44986S

    Committee/Subcommittee: E01.21

    DOI: 10.1520/STP44986S


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