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ASTM Selected Technical Papers
Fracture Mechanics: Fifteenth Symposium
By
RJ Sanford
RJ Sanford
1Department of Mechanical Engineering,
University of Maryland
,
College Park, Maryland
;
symposium chairman and editor
Search for other works by this author on:
ISBN-10:
0-8031-0208-9
ISBN:
978-0-8031-0208-8
No. of Pages:
771
Publisher:
ASTM International
Publication date:
1984

From an engineering view, it is convenient to separate the total fatigue life of notched members into two portions: crack initiation, which is spent nucleating and growing small cracks, and the crack propagation life, which is spent growing these cracks to final fracture. The difficulty in applying this concept has been in defining the size of an initiated crack in a smooth specimen and dealing with small crack growth in the plastic zone near the notch root.

These difficulties may be overcome by considering a simple model where the total fatigue life is the summation of the portion of life controlled by notch plasticity and the portion controlled by nominal stress and crack length. The local strain approach is used to compute the initiation life. Growth of small cracks in the notch plastic zone is assumed to be part of the initiation life. Fracture mechanics concepts are employed to estimate crack propagation lives assuming an initial crack size equal to the notch depth.

Twelve sets of fatigue data reported in the literature were analyzed to assess the validity of the model. These include variations in specimen type, notch size, notch acquity, and material properties. Good correlation between the analytical estimate and experimental data was observed.

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Wetzel
,
R. M.
, Ed.,
Fatigue under Complex Loading: Analysis and Experiments
,
Society of Automotive Engineers
,
Warrendale, Pa.
,
1977
.
2.
Morrow
,
J.
and
Socie
,
D. F.
The Evolution of Fatigue Crack Initiation Life Prediction Methods
,” in
Fatigue 81
,
Society of Environmental Engineers
,
England
,
1981
, pp. 3-21.
3.
Design of Fatigue and Fracture Resistant Structures
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Abelkis
P. R.
and
Hudson
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American Society for Testing and Materials
,
1982
.
4.
Fracture and Fatigue Control in Structures
,
Rolfe
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and
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,
Prentice-Hall
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5.
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An Improved Method of Collocation for the Stress Analysis of Cracked Plates with Various Shaped Boundaries
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08
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6.
Emery
,
A. F.
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Stress Intensity Factor for Edge Cracks in Rectangular Plates with Arbitrary Loadings
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,
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Neuber
,
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,
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8.
Seeger
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,
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Wilson
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,
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10.
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, ASTM STP 462,
American Society for Testing and Materials
,
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11.
Sumpter
,
J. D. G.
and
Turner
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Fracture Analysis in Areas of High Nominal Strain
,” presented at
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,
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,
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12.
Paris
,
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,
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,
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,
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Frost
,
N. E.
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, pp. 109-119.
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Frost
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and
Dugdale
,
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,
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Frost
,
N. E.
,
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,
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16.
Cox
,
E. P.
and
Lawrence
,
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American Society for Testing and Materials
,
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, pp. 529-551.
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Dowling
,
N. E.
,
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, Vol.
2
, No.
2
,
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, pp. 129-138.
18.
Dowling
,
N. E.
and
Wilson
,
W. K.
Analysis of Notch Strain for Cyclic Loading
,” presented at
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, in
Reactor Technology
,
West Berlin, Germany
,
08
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, Vol.
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, Paper L13/4.
19.
Dowling
,
N. E.
and
Wilson
,
W. K.
, “
Geometry and Size Requirements for Fatigue Life Similitude among Notched Members
,” presented at
Fifth International Conference on Fracture
,
Cannes, France
,
03
1981
, in
Advances in Fracture Research
, Vol.
2
,
Francois
E.
, Ed.,
Pergamon Press
,
New York
,
1982
, pp. 581-588.
20.
Raske
,
D. T.
, “
Section and Notch Size Effects in Fatigue
,” TAM Report 360,
College of Engineering, University of Illinois at Urbana-Champaign
,
1972
.
21.
Sehitoglu
,
H.
, “
Fatigue of Low Carbon Steels as Influenced by Repeated Strain Aging
,” Fracture Control Program Report 40,
College of Engineering, University of Illinois at Urbana-Champaign
,
1981
.
22.
Kurath
,
P.
,
Socie
,
D. F.
, and
Morrow
,
JoDean
, “
A Nonarbitrary Fatigue Crack Size Concept to Predict Total Fatigue Lives
,” AFFDL-TR-79-3144,
Wright-Patterson AFB
,
Ohio
,
1979
.
23.
Topper
,
T. H.
,
Wetzel
,
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, and
Morrow
,
JoDean
,
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 0022-2453, Vol.
4
, No.
1
,
1969
, pp. 200-209.
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