Abstract
Fatigue tests of 7075-T6 aluminum alloy under synchronous pulsating triaxial stresses were performed with three different values of the intermediate principal stress. Thick-walled tubes were subjected to internal pressure plus axial stress such that the state of stress at the inner surface was as follows: in the first case, the intermediate principal stress was a compression equal to the internal pressure; in the second, it was a tension equal to the internal pressure; and in the third, it was a tension equal to the hoop stress at the inner surface. Results showed no effect of the intermediate principal stress.
Issue Section:
Research Papers
Keywords:
aluminum alloy,
combined stress,
failure theory,
fatigue,
principal stress,
tresca,
triaxial,
triaxial fatigue
References
1.
Blass
, J. J.
and Findley
, W. N.
, “The Influence of the Intermediate Principal Stress on Fatigue under Triaxial Stresses
,” Materials Research and Standards
0025-5394, MTRSA, Vol. 7
, No. 6
, 06
1967
, pp. 254
-261
.2.
Moore
, R. L.
, Nordmark
, G. E.
, Kaufman
, J. G.
, “Fatigue and Fracture Characteristics of Aluminum Alloy Cylinders under Internal Pressure
,” Alcoa Research Laboratory, Engineering Design Division
, Report 12-70-10, 04
1970
.3.
Morrison
, J. L. M.
, Crossland
, B.
, and Parry
, J. S. C.
, “Strength of Thick Cylinders Subjected to Repeated Internal Pressure
,” Proceedings of the Institution of Mechanical Engineers
, Vol. 174
, 1960
, p. 95.4.
Grover
, H. J.
, “Fatigue of Aircraft Structures
,” Naval Air Systems Command, Department of the Navy, Superintendent of Documents
, Washington, D.C.
, 1966
, pp. 320
-322
.
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