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NASA NTRS · 19880001782

3D inelastic analysis methods for hot section components

Abstract

The objective is to develop analytical tools capable of economically evaluating the cyclic time dependent plasticity which occurs in hot section engine components in areas of strain concentration resulting from the combination of both mechanical and thermal stresses. Three models were developed. A simple model performs time dependent inelastic analysis using the power law creep equation. The second model is the classical model of Professors Walter Haisler and David Allen of Texas A and M University. The third model is the unified model of Bodner, Partom, et al. All models were customized for linear variation of loads and temperatures with all material properties and constitutive models being temperature dependent.

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BibTeXRIS

Dame, L. T., Chen, P. C., Hartle, M. S., Huang, H. T.. 1985-10-01. 3D inelastic analysis methods for hot section components. https://ntrs.nasa.gov/citations/19880001782

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