The Influence of Surface Residual Stress on Fatigue Limit of Titanium-Reference-Cited by-同舟云学术

The Influence of Surface Residual Stress on Fatigue Limit of Titanium

Published:1960-02-01 Issue:1 Volume:82 Page:76-78
ISSN:0022-0817
Container-title:Journal of Engineering for Industry
language:en
Short-container-title:

Author:

Reed E. C.¹,Viens J. A.¹

Affiliation:

1. Pratt & Whitney Aircraft Division, United Aircraft Corporation, East Hartford, Conn.

Abstract

Investigation of the effect of surface residual stress on the endurance limit of 6Al 4V titanium alloy shows that this effect is equal within experimental error to the residual stress divided by a constant. Results can be expressed by a simple equation. A value for the constant has been derived.

Publisher

ASME International

Subject

General Medicine

Link

http://asmedigitalcollection.asme.org/manufacturingscience/article-pdf/82/1/76/6494298/76_1.pdf

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