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High temperature stress-strain analysis (Document No: 19870001776)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Thompson, R. L. |
| Copyright Year | 1984 |
| Description | 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. |
| File Size | 3508323 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870001776 |
| Archival Resource Key | ark:/13960/t0kt1j264 |
| Language | English |
| Publisher Date | 1984-10-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Temperature Distribution Creep Properties Life Durability Linings Performance Prediction Plastic Deformation Burners Design Analysis Finite Element Method Stress-strain Relationships Strain Measurement Prediction Analysis Techniques Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
