Effect of preliminary corrosion on the fatigue strength of an aluminum alloy D16

  • A. V. Karlashov
  • A. D. Gnatyuk
  • N. F. Voronkin
Article
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Abstract

An experimental study of the effect of corrosion on the subsequent fatigue and corrosion-fatigue strength of an aluminum alloy D16 showed that both the fatigue limit and endurance of this alloy are reduced by corrosion in working media characteristic of certain special aviation applications.

Keywords

Aluminum Fatigue Experimental Study Aluminum Alloy Fatigue Strength 

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References

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    A. V. Karlashov and A. D. Gnatyuk, FKhMM [Soviet Materials Science], no. 2, 1966.Google Scholar

Copyright information

© The Faraday Press, Inc. 1968

Authors and Affiliations

  • A. V. Karlashov
    • 1
  • A. D. Gnatyuk
    • 1
  • N. F. Voronkin
    • 1
  1. 1.Kiev Institute of Civil AviationUSSR

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