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ASTM Selected Technical Papers
Low Cycle Fatigue
By
HD Solomon
HD Solomon
1
General Electric Corporate Research and Development Center
,
Schenectady, New York
;
symposium chairman and co-editor
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GR Halford
GR Halford
2
NASA-Lewis Research Center
,
Cleveland, Ohio
;
co-editor
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LR Kaisand
LR Kaisand
3
General Electric Corporate Research and Development Center
,
Schenectady, New York
;
symposium chairman and co-editor
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BN Leis
BN Leis
4
Battelle Columbus Laboratories
,
Columbus, Ohio
;
co-editor
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ISBN-10:
0-8031-0944-X
ISBN:
978-0-8031-0944-5
No. of Pages:
1307
Publisher:
ASTM International
Publication date:
1988

There has been special interest recently in developing new, reliable analytical design methods for components under higher temperature conditions. However, at present, the use of material properties is still limited to arrays of single characteristics which do not interact with each other. In this work, several creep fatigue experiments on smooth specimens of IN 800 H have been carried out at 830°C. In some tests, these have also been combined with inside hysteresis loops to investigate the different effects on deformation and damage behavior which originate in a creep and fatigue environment. As a result of these tests, it has been found that the material behavior under creep-fatigue conditions can be significantly changed compared to the material behavior under simple load conditions. Therefore there is a need for life analysis methods to be expanded to include possible variations in properties; for greater accuracy, the material properties must be treated as a complex interacting system of parameters. The examination has been extended to a typical component used under high-temperature conditions. The results of the numerical analysis show that the stress-strain history in the critical area of that component is not simply strain controlled, as it is in the typical laboratory creep-fatigue interaction life test containing a tensile or compressive dwell at constant peak strain level. At high temperatures, the conditions in the component are more severe, causing the life to be reduced compared with the typical laboratory test. In this paper, these conditions are successfully simulated with the help of a generalized Neuber law: σ · εp = constant. Based on this ratio, the engineering method for evaluating component geometry and loading conditions and their effects on material behavior can be established.

On the basis of the results of this study, it follows that a very large amount of information on material behavior and on its component dependence is needed when the material properties are time-dependent, as in the design of hot components. For that reason, the satisfactory solution to designing components for high-temperature conditions requires an integrated approach, with full consideration of different interaction effects from the various influences in the main areas of the material deformation and damage behavior, and of the component effects. The results of this study may apply to the standard methodology of life prediction in high-temperature areas, which shall be developed in the future.

1.
Manson
,
S. S.
,
Halford
,
G. R.
, and
Hirschberg
,
M. H.
, “
Creep-Fatigue Analysis by Strain-Range Partitioning
,”
NASA Technical Memorandum
 TM X-67838,
National Aeronautics and Space Administration
,
Washington, D.C.
,
06
1971
.
2.
Hirshberg
,
M. H.
and
Halford
,
G. R.
, “
Use of Strain Range Partitioning to Predict High-Temperature Low Cycle Fatigue Life
,”
NASA Technical Note
 TN D-8072,
National Aeronautics and Space Administration
,
Washington, D.C.
,
01
1976
.
3.
Jaske
,
C. E.
,
Midlin
,
H.
, and
Perrin
,
J. S.
, “
Combined Low-Cycle Fatigue and Stress Relaxation of Alloy 800 and Type 304 Stainless Steel at Elevated Temperatures
,” in
Fatigue at Elevated Temperature
, ASTM STP 520,
American Society for Testing and Materials
,
Philadelphia
,
1973
, pp. 365-376.
4.
ASME Boiler and Pressure Vessel Code Cases, Case N-47 (1592)
,”
Class 1 Components in Elevated Temperature Service
, Section III, Division 1,
American Society of Mechanical Engineers
,
New York
,
1979
.
5.
Coffin
,
L. F.
, “
Fatigue at High Temperature
,”
Technical Information Series Report
72CRD135,
General Electric
, Schenectady, N.Y.,
04
1972
.
6.
Saltsman
,
J. F.
and
Halford
,
G. R.
, “
Application of Strain Range Partitioning to the Prediction of MPC Creep-Fatigue Data for 2¼Cr-1Mo Steel
,”
NASA Technical Memorandum
 TM X-73474,
National Aeronautics and Space Administration
,
Washington, D.C.
,
12
1976
.
7.
Lawton
,
C. W.
, “
Use of Low-Cycle Fatigue Data for Pressure Vessel Design
,” in
Low-Cycle Fatigue and Life Prediction
, ASTM STP 770,
American Society for Testing and Materials
,
Philadelphia
,
1982
, pp. 585-599.
8.
Agatonovic
,
P.
in
Proceedings
,
Second International Conference on Creep and Fracture of Engineering Materials and Structures
,
Wilshire
B.
and
Owne
D. R.
, Eds.,
Pineridge Press
,
Swansea, U.K.
,
1984
, pp. 1079-1090.
9.
Agatonovic
,
P.
and
Heidenreich
,
R.
in “
Werkstoffprüfung 1984
,” DVM
1985
(250),
Deutscher Verband für Materialprüfung e.V.
,
Berlin, West Germany
,
1985
, pp. 477-488.
10.
Agatonovic
,
P.
and
Dogigli
,
M.
in
Proceedings
,
Fourth International Conference on Numerical Methods in Thermal Problems
,
Lewis
R. W.
, Ed.,
Pineridge Press
,
Swansea, U.K.
,
1985
.
11.
Walcher
,
J.
and
Gray
,
D.
, “
Aspects of Cumulative Fatigue Damage Analysis of Cold End Rotation Structures
,”
AIAA/SAE/ASME 15th Joint Propulsion Conference
, 18–20 June 1979,
Las Vegas
, Nev.
12.
Cruse
,
T. A.
and
Meyer
,
T. G.
, “
Structural Life Prediction and Analysis Technology
, Report FR-10896,
Pratt and Whitney Aircraft Group
,
03
11
1978
.
13.
Walker
,
K. P.
, “
Research and Development Program for Nonlinear Structural Modelling with Advanced Time-Temperature Dependent Constitutive Relationship
,” NASA Report CR-165533,
National Aeronautics and Space Administration
, Washington, D.C.,
11
1981
.
14.
Hart
,
E. W.
,
ASME Journal of Engineering Materials and Technology
, Vol.
98
,
1976
, pp. 193-202.
15.
Mottot
,
M.
,
Petrequin
,
P.
,
Amzallag
,
C.
,
Rabbe
,
P.
,
Grattier
,
J.
, and
Masson
,
S.
, “
Behavior in Fatigue-Relaxation of High-Creep Resistant Type 316L Stainless Steel
” in
Low-Cycle Fatigue and Life Prediction
, ASTM STP 770,
American Society for Testing and Materials
,
Philadelphia
,
1982
, pp. 152-168.
16.
Morrow
,
J. D.
,
Wetzel
,
R. M.
, and
Topper
,
T. H.
, “
Laboratory Simulation of Structural Fatigue Behavior
” in
Effects of Environment and Complex Load History on Fatigue Life
, ASTM STP 462,
American Society for Testing and Materials
,
Philadelphia
,
1970
, pp. 74-91.
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