NASA NTRS · 19890007950
Three-dimensional inelastic analysis methods for hot section components
Abstract
The objective was to develop analytical methods capable of evaluating the cyclic time dependent inelasticity which occurs in hot section engine components. Because of the large excursions in temperature associated with hot section engine components, the techniques developed must be able to accommodate large variations in material behavior including plasticity and creep. To meet this objective, a matrix consisting of three constitutive mode-element formulations was developed. A separate program for each combination of constitutive mode-element model was written. The source codes of the nine programs range in size from 7300 lines for the Bodner/twenty code to 19,000 lines for the Haisler and Allen/nine code. All the codes were given a stand alone capability of performing cyclic nonlinear analysis.
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Lackney, Joseph, Chamis, C. C.. 1987-10-01. Three-dimensional inelastic analysis methods for hot section components. https://ntrs.nasa.gov/citations/19890007950
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