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ASTM Selected Technical Papers
Cyclic Stress-Strain Behavior—Analysis, Experimentation, and Failure Prediction
By
LF Coffin, Jr. Jr.
LF Coffin, Jr. Jr.
1
Corporate Research & Development Center, General Electric Company
,
Schenectady, N.Y.
Search for other works by this author on:
E Krempl
E Krempl
2Mechanics Division,
Rensselaer Polytechnic Institute
,
Troy, N.Y.
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ISBN-10:
0-8031-0078-7
ISBN:
978-0-8031-0078-7
No. of Pages:
290
Publisher:
ASTM International
Publication date:
1971

Constant amplitude fatigue tests with various conditions of overloads were conducted to understand the effects of load interaction and sequence in notched coupons. The results were analyzed with particular emphasis on the local residual stresses at notches. Fatigue life results from the tests having a variation in the number of cycles between the periodic overloads which reinforce the concept of a fading residual stress. Other fatigue life trends could be predicted by assuming a stable residual stress. Conditions which could cause cycle-dependent overload residual stresses are discussed. An exponential analysis form is suggested for calculating the cycle-dependent local stresses for application to cumulative damage predictions.

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Heywood
,
R. B.
in
Colloquium on Fatigue
,
Springer-Verlag
,
1956
, pp. 92–102.
2.
Mordfin
,
L.
and
Halsey
,
N.
in
Fatigue Tests of Aircraft Structures: Low-Cycle, Full-Scale, and Helicopters
, ASTM STP 338,
American Society for Testing and Materials
,
1963
, pp. 251–272.
3.
Breyan
,
W.
in
Effects of Environment and Complex Load History on Fatigue Life
, ASTM STP 462,
American Society for Testing and Materials
,
1970
, pp. 127–166.
4.
Kessler
,
A. F.
and
Hillberry
,
B. M.
, “
The Effect of Periodic Overstress on the Fatigue Life of Notched Aluminum Specimens
,” SAE Paper 710599,
Society of Automotive Engineers
,
New York
,
06
1971
.
5.
Neuber
,
H.
,
Transactions of the ASME, Journal of Applied Mechanics
,
12
1961
, p. 544.
6.
Wetzel
,
R. M.
,
Journal of Materials
, Vol.
3
, No.
3
,
09
1968
, p. 646.
7.
Wetzel
,
R. M.
,
Morrow
,
JoDean
, and
Topper
,
T. H.
, “
Fatigue of Notched Parts with Emphasis on Local Stresses and Strains
,” NADC-ST-6818,
Naval Air Development Center
, Johnsville, Pa.,
09
1968
.
8.
Potter
,
J. M.
, “
A Simple Graphical Procedure for Determining Cyclic Elasto-Plastic Notch Stresses
,”
AIAA Journal, American Institute of Aeronautics and Astronautics
 0001-1452, Vol.
10
, No.
10
,
10
1972
, p. 1304.
9.
Potter
,
J. M.
, “
A General Fatigue Prediction Method Based on Neuber Notch Stresses and Strains
,” AFFDL-TR-70-161,
Air Force Flight Dynamics Laboratory
, (AD 723631) Dayton, Ohio,
02
1971
.
10.
Crews
,
J. H.
, Jr.
, “
Local Plastic Stresses in Sheet Aluminum Alloy Specimens with Stress Concentration Factor of 2 Under Constant-Amplitude Loading
,” NASA TN D-3152,
12
1965
.
11.
Crews
,
J. H.
, Jr.
, “
Elasto Plastic Stress-Strain Behavior at Notch Root in Sheet Specimens Under Constant-Amplitude Loading
,” NASA TN D-5253,
06
1969
.
12.
Peterson
,
R. E.
,
Stress Concentration Design Factors
,
Wiley
,
New York
,
1953
.
13.
Metallic Materials and Elements for Aerospace Vehicle Structures
, MIL-HDBK-5A,
Department of Defense
,
Washington, D. C.
,
02
1966
.
14.
Stadnick
,
S. J.
, “
Simulation of Overload Effect in Fatigue Based on Neuber's Analysis
,” Report 325,
Department of Theoretical and Applied Mechanics, University of Illinois
, Urbana, Ill.,
1969
.
15.
Morrow
,
JoDean
,
Ross
,
A. S.
, and
Sinclair
,
G. M.
,
Transactions, Society of Automotive Engineers
, Vol.
68
,
1960
, pp. 40–48.
16.
Rosenthal
,
D.
and
Sines
,
G.
,
Proceedings, American Society for Testing and Materials
, Vol.
51
,
1951
, p. 593.
17.
Impellizzeri
,
L. F.
in
Effects of Environment and Complex Load History on Fatigue Life
, ASTM STP 462,
American Society for Testing and Materials
,
1970
, pp. 40–68.
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