TECHNICAL PAPERS
Oct 1, 1993

Probabilistic Material Degradation under High Temperature, Fatigue, and Creep

Publication: Journal of Aerospace Engineering
Volume 6, Issue 4

Abstract

This paper describes the development of methodology that provides for quantification of uncertainty in the lifetime material strength degradation of structural components of aerospace propulsion systems subjected to a number of diverse random effects. The methodology is embodied in the two computer programs PROMISS and PROMISC. These programs form a material‐resistance model used in an aerospace structural‐reliability program NESSUS. A probabilistic material‐degradation model, in the form of a postulated randomized multifactor interaction equation, is used to quantify lifetime material strength. Each multiplicative term in the model has the property that if the current value of an effect equals the ultimate value, then the lifetime strength will be zero. Also, if the current value of an effect equals the reference value, the term equals one and lifetime strength is not affected by that particular effect. Presently, the model includes three effects that typically reduce lifetime strength: high temperature, mechanical fatigue, and creep. The paper also includes the statistical analysis of experimental data for INCONEL 718 obtained from the open literature. This statistical analysis of data provided regression parameters for use as the empirical material constants of the model, thus calibrating the model specifically for INCONEL 718. Model calibration was carried out for three variables, namely, high temperature, mechanical fatigue, and creep. Finally, using the PROMISS computer program, a sensitivity study was performed with the calibrated random model illustrating the effect of each variable upon random lifetime strength.

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References

1.
Barker, J. F., Ross, E. W., and Radavich, J. F. (1970). “Long time stability of INCONEL 718.” J. Metals, 22(Jan.), 32.
2.
Boyce, L., and Chamis, C. C. (1989). “Probablistic constitutive relationships for material strength degradation models.” Proc., 30th Structures, Structural Dynamics and Materials Conf., 1832‐1839.
3.
Boyce, L., Keating, J., Lovelace, T., and Bast, C. (1990). Probabilistic lifetime strength of aerospace materials via computational simulations: NASA CR 187178. Nat. Aeronautics and Space Admin., Washington, D.C.
4.
Chamis, C. C. (1984). Simplified composite micromechanics equations for strength, fracture toughness, impact resistance and environmental effects: NASA TM 83696. Nat. Aeronautics and Space Admin., Washington, D.C.
5.
Chamis, C. C., and Hopkins, D. (1985). Thermoviscoplastic nonlinear constitutive relationships for structural analysis of high temperature metal matrix composites: NASA TM 87291. Nat. Aeronautics and Space Admin., Washington, D.C.
6.
Cullen, T. M., and Freeman, J. W. (1985). The mechanical properties of INCONEL 718 sheet alloy at 800°, 1000° and 1200°F: NASA CR 268. Nat. Aeronautics and Space Admin., Washington, D.C.
7.
Hopkins, D. A. (1984). Nonlinear analysis for high‐temperature multilayered fiber composite structures: NASA TM 83754. Nat. Aeronautics and Space Admin., Washington, D.C.
8.
Hopkins, D., and Chamis, C. C. (1985). A unique set of micromechanics equations for high temperature metal matrix composites: NASA TM 87154. Nat. Aeronautics and Space Admin., Washington, D.C.
9.
INCONEL Alloy 601. (1988). Inco Alloys Int., Inc., Huntington, W.V., 5.
10.
INCONEL Alloy 718. (1986). Inco Alloys Int., Inc., Huntington, W.V., 8, 13.
11.
INCONEL Alloy X‐750. (1979). Huntington Alloys, Inc., Huntington, W.V., 5, 7.
12.
Petrasek, D. W. (1979). Tungsten wire‐reinforced superalloys for 1093°C turbine blade applications: NASA CR 159720. Nat. Aeronautics and Space Admin., Washington, D.C., 13.
13.
Petrasek, D. W., and Titran, R. H. (1988). Creep behavior of tungsten/niobium and tungsten/niobium‐1 percent zirconium composites: NASA TM 100804. Nat. Aeronautics and Space Admin., Washington, D.C., 16–17.
14.
Ross, S. M. (1987). Introduction to probability and statistics for engineers and scientists. John Wiley and Sons, New York, N.Y., 278.
15.
Scott, D. W. (1976). Nonparametric probability density estimation by optimization theoretic techniques: NASA CR 147763. Nat. Aeronautics and Space Admin., Washington, D.C.
16.
Siddall, J. N. (1982). “A comparison of several methods of probabilistic modeling.” Proc. ASME Computers in Engineering Conference, ASME, New York, N.Y., 4, 231–238.
17.
Sims, C. T., Stoloff, N. S., and Hagel, W. C. (1987). Superalloys II. John Wiley and Sons, New York, N.Y., 581–585, 590–595.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 6Issue 4October 1993
Pages: 347 - 362

History

Received: Oct 30, 1991
Published online: Oct 1, 1993
Published in print: Oct 1993

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Authors

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L. Boyce
P.E., Assoc. Prof. of Mech. Engrg., Div. of Engrg., The Univ. of Texas at San Antonio, San Antonio, TX 78249

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