NASA NTRS · 19860002050
The 3-D inelastic analysis methods for hot section components (base program)
Abstract
The objective of this program is to produce a series of new computer codes that permit more accurate and efficient three dimensional inelastic analysis of selected hot section components - combustor liners, turbine blades and turbine vanes. The computer codes embody a progression of mathematical models and are streamlined to take advantage of geometrical features, loading conditions, and forms of material response that distinguish each group of selected components.
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Todd, E. S.. 1983-10-01. The 3-D inelastic analysis methods for hot section components (base program). https://ntrs.nasa.gov/citations/19860002050
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