The effect of high loads on fatigue

  • R. B. Heywood
Conference paper
Part of the IUTAM Symposia book series (IUTAM)

Abstract

At first sight, it might be thought that occasional high loads would have little influence on fatigue, so long as the damage as indicated by the cumulative damage rule was small. This supposition is supported by results of tests made at the Aluminium Laboratories [1] on plain aluminium alloy specimens, when a single initial stretch in axial tension slightly reduced the fatigue strength in rotating bending, the maximum reduction being 12%, see table 1.

Keywords

Fatigue Sine Tria Strain Hardening 

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Bibliography

  1. [1]
    Teed, P. L.: Aeroplane 82, 787 (1952).Google Scholar
  2. [2]
    Forrest, G.: J. Inst. Metals 72, 1–17 (1946); also: J. Roy. aeronaut. Soc. 58, 261–276 (1954).Google Scholar
  3. [3]
    Rosenthal, D., and G. Sines: Proc. ASTM 51, 593–610 (1951) (Discussion by Templin).Google Scholar
  4. [4]
    Kerry, F. A., J. Nichols and K. Vincent: Saunders-Roe Ltd Rep. (England) SR/S/762 (1952).Google Scholar
  5. [5]
    Walker, P. B.: J. Roy. aeronaut. Soc, 57, 12 (1953).Google Scholar

Copyright information

© Springer-Verlag OHG., Berlin · Gottingen · Heidelberg 1956

Authors and Affiliations

  • R. B. Heywood

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