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ASTM Selected Technical Papers
Effects of Environment and Complex Load History on Fatigue LifeAvailable to Purchase
By
MS Rosenfeld
MS Rosenfeld
1
Research Aerospace Engineer
, Aero Structures Department,
Naval Air Development Center
;
symposium chairman
.
Search for other works by this author on:
ISBN-10:
0-8031-0032-9
ISBN:
978-0-8031-0032-9
No. of Pages:
334
Publisher:
ASTM International
Publication date:
1970

The fatigue behavior of high-purity nickel, vibrated in reversed bending, was studied at 300 C in oxygen and in water vapor at pressures from 10-9 to 10 torr. Fatigue life was reduced in both oxygen and water vapor, but the variation in life with pressure differed somewhat for the two. The curve of fatigue life versus oxygen pressure is step-shaped with little or no dependence of life on pressure at very low and high pressures, the major reduction taking place at intermediate pressures. In contrast, the fatigue life in water vapor drops off gradually throughout the entire high-pressure range, but the maximum reduction is much less than in oxygen. Evidence obtained by residual gas analysis shows that a hot ionization gage filament may change the composition of the environment which, in turn, may affect fatigue life. Metallographic examination of failed specimens disclosed a relation between deformation and cracking characteristics and oxygen pressure. A calculation of the pressure required to saturate the crack surfaces at an estimated rate of crack growth showed that the predicted pressure agreed with the highest transition pressure, at which the reduction in fatigue life approaches a maximum.

1.
Wadsworth
,
N. J.
and
Hutchings
,
J.
, “
The Effect of Atmospheric Corrosion on Metal Fatigue
,”
Philosophical Magazine
 1478-6435, Vol.
3
, No.
34
, October, 1958, p. 1154.
2.
Snowden
,
K. U.
, “
The Effect of Atmosphere on the Fatigue of Lead
,”
Acta Metallurgica
 0001-6160, Vol.
12
,
1964
, p. 295.
3.
Bradshaw
,
F. J.
and
Wheeler
,
C.
, “
The Effect of Environment on Fatigue Crack Growth in Aluminum and Aluminum Alloys
,”
Applied Materials Research
 0570-4847, Vol.
5
,
1966
, p. 112.
4.
Hartman
,
A.
, “
On the Effect of Oxygen and Water Vapor on the Propagation of Fatigue Cracks in 2024-T3 Alclad Sheet
,”
International Journal of Fracture Mechanics
, Vol.
1
, No.
3
, September, 1965, p. 167.
5.
Broome
,
T.
and
Nicholson
,
A.
, “
Atmospheric Corrosion—Fatigue of Age-Hardened Aluminum Alloys
,”
Journal, Institute of Metals
, Vol.
89
, 1960–61, p. 183.
6.
Achter
,
M. R.
,
Smith
,
H. H.
,
Riley
,
R. J.
, and
Stegman
,
R. L.
, “
Flexural Fatigue Machine for High Temperature Operation at Resonance in Vacuum
,”
The Review of Scientific Instruments
 0034-6748, Vol.
37
,
1966
, p. 311
7.
Danek
,
G. J.
, Jr.
,
Smith
,
H. H.
, and
Achter
,
M. R.
, “
High Temperature Fatigue and Bending Strain Measurements in Controlled Environments
,”
Proceedings, American Society for Testing and Materials
, Vol.
61
,
1961
, p. 775.
8.
Hickmott
,
T. W.
and
Ehrlich
,
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, “
Interaction of Hydrogen with Tungsten
,”
Journal of Physics and Chemistry of Solids
 0022-3697, Vol.
5
,
1958
, p. 47.
9.
Forsyth
,
P. J. E.
and
Stubbington
,
C. A.
, “
The Slip-Band Extrusion Effect Observed in Some Aluminum Alloys Subjected to Cyclic Stresses
,”
Journal, Institute of Metals
, Vol.
83
, 1954–55, p. 395.
10.
Smith
,
H. H.
,
Shahinian
,
P.
, and
Achter
,
M. R.
, “
Fatigue Crack Growth Rates in Type 316 Stainless Steel at Elevated Temperatures as a Function of Oxygen Pressure
,”
Transactions, Metallurgical Society, American Institute of Mining, Metallurgical, and Petroleum Engineers
, Vol.
245
,
1969
, p. 947.
11.
Sumsion
,
H. T.
, “
Effect of High Vacuum on the Fatigue Properties of Magnesium and Two Magnesium Alloys
,” ASTM/IES/AIAA Second Space Simulation Conference Proceedings,
American Society for Testing and Materials
, September, 1967, p. 91.
12.
Burnett
,
S. C.
, Naval Research Laboratory, private communication.
13.
Santeler
,
D. J.
,
Jones
,
D. W.
,
Holkeboer
,
D. H.
, and
Pagano
,
F.
, “
Vacuum Technology and Space Simulation
,” NASA SP-105,
National Aeronautics and Space Administration
,
1966
, p. 184.
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