NASA NTRS · 19890003545
Life prediction and constitutive models for engine hot section
Abstract
The purpose of this program is to develop life prediction models for coated anisotropic materials used in gas turbine airfoils. In the program, two single crystal alloys and two coatings are being tested. These include PWA 1480, Alloy 185, overlay coating (PWA 286), and aluminide coating (PWA 273). Constitutive models are also being developed for these materials to predict the time independent (plastic) and time dependent (creep) strain histories of the materials in the lab tests and for actual design conditions. This nonlinear material behavior is particularly important for high temperature gas turbine applications and is basic to any life prediction system. Some of the accomplishments of the program are highlighted.
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Swanson, G. A., Meyer, T. G., Nissley, D. M.. 1986-10-01. Life prediction and constitutive models for engine hot section. https://ntrs.nasa.gov/citations/19890003545
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