NASA NTRS ยท 19870001776
High temperature stress-strain analysis
Abstract
The objectives are threefold: to assist in developing predictive tools needed to improve design analyses and procedures for the efficient and accurate prediction of burner liner structural performance and response; to calibrate, validate, and evaluate these predictive tools by comparing the predicted results with the experimental data; and to evaluate existing as well as advanced temperature and strain measurement instrumentation, through both contact and noncontact efforts, in a simulated turbine engine combustor environment. As the predictive tool, tests, test methods, instrumentation, and data acquisition and reduction methods are developed and evaluated, a proven, integrated analysis/experiment method will be developed that will permit the accurate prediction of the cyclic life of a burner liner.
Keep this discovery
Explore connections, maps & timelines
Thompson, R. L.. 1984-10-01. High temperature stress-strain analysis. https://ntrs.nasa.gov/citations/19870001776
Cite the original work for its findings. Save a collection to share your selection of sources.