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NASA NTRS · 19860002049

The 3D inelastic analysis methods for hot section components

Abstract

The objective of this research is to develop an analytical tool 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. The techniques developed must be capable of accommodating large excursions in temperatures with the associated variations in material properties including plasticity and creep. The overall objective of this proposed program is to develop advanced 3-D inelastic structural/stress analysis methods and solution strategies for more accurate and yet more cost effective analysis of combustors, turbine blades, and vanes. The approach will be to develop four different theories, one linear and three higher order with increasing complexities including embedded singularities.

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BibTeXRIS

Dame, L. T., Mcknight, R. L.. 1983-10-01. The 3D inelastic analysis methods for hot section components. https://ntrs.nasa.gov/citations/19860002049

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