Effect of range of stress in combined bending and torsion fatigue tests of 25S T aluminum alloy
Findley, W.N.; Mitchell, W.I.; Strohbeck, D.D.
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https://hdl.handle.net/2142/112306
Description
Title
Effect of range of stress in combined bending and torsion fatigue tests of 25S T aluminum alloy
Author(s)
Findley, W.N.
Mitchell, W.I.
Strohbeck, D.D.
Issue Date
1954-04
Keyword(s)
Stress
Bending
Torsion
Fatigue Tests
Aluminum Alloy
Abstract
Fatigue test data under bending, torsion, and combined
bending and torsion are presented for mean stresses from zero
to values which caused substantial yielding . The mean normal
stresses in the bending and the torsion tests were corrected
for the effect of the non linear distribution of stress result
ing from yielding. The effect of stress relaxation at high mean
stresses was investigated . The applicability of several theories
of failure are compared wit h these t est data. The influence o~
anisotropy, mechanism of crack formation, mean stress and maxi.
mum stress are discussed.
Publisher
Department of Theoretical and Applied Mechanics. College of Engineering. University of Illinois at Urbana-Champaign
Series/Report Name or Number
TAM R 57
1967-0354
ISSN
0073-5264
Type of Resource
text
Language
eng
Permalink
http://hdl.handle.net/2142/112306
Sponsor(s)/Grant Number(s)
Office of Ordnance Research, Ordnance Corps, Department of the Army, Contract No. DA-11-022-ORD-995, Project No. TB2-0001(313)
Copyright and License Information
Copyright 1954 Board of Trustees of the University of Illinois
TAM technical reports include manuscripts intended for publication, theses judged to have general interest, notes prepared for short courses, symposia compiled from outstanding undergraduate projects, and reports prepared for research-sponsoring agencies.
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