NASA NTRS ยท 19870046371
Advances in 3-D Inelastic Analysis Methods for hot section components
Abstract
3-D Inelastic Analysis Methods are described. These methods consist of a series of new computer codes embodying a progression of mathematical models (mechanics of materials, specialty 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 paper.
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Chamis, Christos C.. 1987-01-01. Advances in 3-D Inelastic Analysis Methods for hot section components. https://ntrs.nasa.gov/citations/19870046371
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