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ASTM Selected Technical Papers
Cyclic Stress-Strain and Plastic Deformation Aspects of Fatigue Crack Growth
By
LF Impellizzeri
LF Impellizzeri
1
Branch Chief
,
Technology-Strength, McDonnell Aircraft Company
,
St. Louis, Mo. 63166
;
symposium chairman
.
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ISBN-10:
0-8031-0319-0
ISBN:
978-0-8031-0319-1
No. of Pages:
231
Publisher:
ASTM International
Publication date:
1977

An elastic-plastic (incremental) finite-element analysis, in conjunction with a crack-growth criterion, was used to study crack-growth behavior under monotonic and cyclic loading. The crack-growth criterion was based on crack-tip strain. Whenever the crack-tip strain equals or exceeds a critical strain value, the crack grows. The effects of element-mesh size, critical strain, strain hardening, and specimen type (tension or bending) on crack growth under monotonic loading were investigated. Crack growth under cyclic loading (constant amplitude and simple variable amplitude) were also studied. A combined hardening theory, which incorporates features of both isotropic and kinematic hardening under cyclic loading, was also developed for smooth yield surfaces and was used in the analysis.

1.
Strawley
,
J. E.
and
Brown
,
W. F.
, Jr.
,
Fracture Toughness Testing and its Applications, ASTM STP 381
,
American Society for Testing and Materials
,
1965
, pp. 133–198.
2.
Elber
,
W.
in
Damage Tolerance in Aircraft Structures, ASTM STP 486
,
American Society for Testing and Materials
,
1970
, pp. 230–242.
3.
Kobayashi
,
A. S.
,
Chiu
,
S. T.
, and
Beeuwkes
,
R.
,
Engineering Fracture Mechanics
, Vol.
5
, No.
2
,
1973
, pp. 293–305.
4.
Anderson
,
Hans
,
International Journal of Fracture
, Vol.
9
,
1973
, pp. 231–233.
5.
Newman
,
J. C.
, Jr.
, “
Finite-Element Analysis of Fatigue Crack Propagation—Including the Effects of Crack Closure
,” Ph.D. Thesis,
Virginia Polytechnic Institute and State University
,
05
1974
.
6.
Newman
,
J. C.
, Jr.
, and
Armen
,
Harry
, Jr.
,
AIAA Journal
, American Institute of Aeronautics and Astronautics, Vol.
14
, No.
8
,
08
1975
, pp. 1017–1023.
7.
Ohji
,
K.
,
Ogura
,
K.
, and
Ohkubo
,
Y.
,
Engineering Fracture Mechanics
, Vol.
7
,
1975
, pp. 457–464.
8.
Newman
,
J. C.
, Jr.
, in
Mechanics of Crack Growth, ASTM STP 590
,
American Society for Testing and Materials
,
1976
, pp. 281–301.
9.
Zienkiewicz
,
O. C.
,
Valliappan
,
S.
, and
King
,
I. P.
,
International Journal for Numerical Methods in Engineering
, Vol.
1
,
1969
, pp. 75–100.
10.
Prager
,
W.
,
Journal of Applied Mechanics
,
12
1956
, pp. 493–496.
11.
Hill
,
R.
,
The Mathematical Theory of Plasticity
, Oxford,
1950
.
12.
Hodge
,
P. G.
, Jr.
, “
Piecewise Linear Plasticity
,” Ninth International Congress of Applied Mechanics, Brussels,
09
1956
.
13.
Hodge
,
P. G.
, Jr.
,
Journal of Applied Mechanics
,
09
1957
, pp. 481–484.
14.
Hunsaker
,
B.
, Jr.
,
Vaughan
,
D. K.
, and
Stricklin
,
J. A.
, “
A Comparision of the Capability of Four Hardening Rules to Predict a Material's Plastic Behavior
,” Transaction of the ASME,
Journal of Pressure Vessel Technology
,
02
1976
.
15.
Neuber
,
H.
, Transactions, American Society of Mechanical Engineers, Series
E.
,
Journal of Applied Mechanics
, Vol.
28
,
1961
, pp. 544–550.
16.
Brown
,
W. F.
, Jr.
, and
Srawley
,
J. E.
,
Plane Strain Crack Toughness Testing of High Strength Metallic Materials, ASTM STP 410
,
American Society for Testing and Materials
,
1966
.
17.
Drucker
,
D. C.
,
Proceedings of the 1st U.S. National Congress on Applied Mechanics
,
1951
, pp. 487–491.
18.
Isakson
,
G.
,
Armen
,
H.
, Jr.
, and
Pifko
,
A.
, “
Discrete-Element Methods for the Plastic Analysis of Structures
,” NASA CR-803,
10
1967
.
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