NASA NTRS · 19870001773
The 3D inelastic analysis methods for hot section components
Abstract
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 are being developed. The approach is to develop four different theories, one linear and three higher order with increasing complexities including embedded singularities. Progress in each area is reported.
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Roberts, M. L., Mcknight, R. L., Dame, L. T., Chen, P. C.. 1984-10-01. The 3D inelastic analysis methods for hot section components. https://ntrs.nasa.gov/citations/19870001773
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