NASA NTRS · 19870003490
On 3-D inelastic analysis methods for hot section components (base program)
Abstract
A 3-D Inelastic Analysis Method program is described. This program consists of a series of new computer codes embodying a progression of mathematical models (mechanics of materials, special finite element, boundary element) for streamlined analysis of: (1) combustor liners, (2) turbine blades, and (3) turbine vanes. These models address the effects of high temperatures and thermal/mechanical loadings on the local (stress/strain)and global (dynamics, buckling) structural behavior of the three selected components. Three computer codes, referred to as MOMM (Mechanics of Materials Model), MHOST (Marc-Hot Section Technology), and BEST (Boundary Element Stress Technology), have been developed and are briefly described in this report.
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Wilson, R. B., Bak, M. J., Nakazawa, S., Banerjee, P. K.. 1986-02-01. On 3-D inelastic analysis methods for hot section components (base program). https://ntrs.nasa.gov/citations/19870003490
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