SEDL / STP / STP174-EB / STP44986S



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


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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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