Effect of overheating on creep-rupture properties of S-816 alloy at 1,500 degrees F Metadata

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  • Main Title Effect of overheating on creep-rupture properties of S-816 alloy at 1,500 degrees F
  • Series Title NACA Technical Notes


  • Author: Rowe, John P.
    Creator Type: Personal
  • Author: Freeman, J. W.
    Creator Type: Personal


  • Originator: United States. National Advisory Committee for Aeronautics.
    Contributor Type: Organization
  • Originator: University of Michigan
    Contributor Type: Organization


  • Creation: 1957-12


  • English


  • Content Description: The effects of overheats to temperatures of 1650, 1800, 1900, and 2000 F were evaluated in terms of the changes in creep-rupture characteristics at 1500 F of S-816 alloy under stresses within the range of rupture strengths of the alloy for 100 to 1000 hours. Overheat periods were predominantly of 2-minute duration and were applied cyclically at approximately 5- or 12-hour intervals. The possible damage from overheating was believed to include internal metal structure changes induced by exposure to the higher temperatures and loss of life by creep if stress was present during the overheats.
  • Physical Description: 75 p. : ill.


  • Keyword: creep-rupture characteristics
  • Keyword: overheating
  • Keyword: alloys


  • Name: National Advisory Committee for Aeronautics Collection
    Code: NACA
  • Name: Technical Report Archive and Image Library
    Code: TRAIL


  • Name: UNT Libraries Government Documents Department
    Code: UNTGD


  • Rights Access: public
  • Rights License: pd
  • Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available

Resource Type

  • Report


  • Text


  • Accession or Local Control No: 93R14389
  • URL: http://hdl.handle.net/2060/19930085099
  • Report No.: NACA-TN-4081
  • Center for AeroSpace Information Number: 19930085099
  • Archival Resource Key: ark:/67531/metadc57081