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Creep fatigue life prediction for engine hot section materials (isotropic) fifth year progress review
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Harvey, Peter R. Nelson, Richard S. |
| Copyright Year | 1987 |
| Description | The need for advanced life prediction methods for hot section components for gas turbine engines is becoming more and more evident. The complex local strain and temperature histories at critical locations must be accurately interpreted to account for the effects of various damage mechanisms and their possible interactions. This program is designed to investigate these fundamental damage processes, identify modeling strategies, and develop practical models which can be used to guide the early design and development of new engines and to increase the durability of existing engines. |
| File Size | 8909622 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890007965 |
| Archival Resource Key | ark:/13960/t7mp9xk9r |
| Language | English |
| Publisher Date | 1987-10-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Isotropy Life Durability Predictions Gas Turbine Engines Thermal Cycling Tests Thermal Fatigue Mathematical Models Damage Engine Parts Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
