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The 3d inelastic analysis methods for hot section components (Document No: 19870001773)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chen, P. C. Dame, L. T. McKnight, R. L. Roberts, M. L. |
| Copyright Year | 1984 |
| Description | Advanced 3-D inelastic structural/stress analysis methods and solution strategies for more accurate and yet more cost-effective analysis of combustors, turbine blades, and vanes are being developed. The approach is to develop four different theories, one linear and three higher order with increasing complexities including embedded singularities. Progress in each area is reported. |
| File Size | 153045 |
| Page Count | 3 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870001773 |
| Archival Resource Key | ark:/13960/t48q0vg9k |
| Language | English |
| Publisher Date | 1984-10-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Temperature Measurement Time Dependence Stress Analysis Creep Properties Stress-strain Relationships Cost Effectiveness Mathematical Models Elastic Properties Turbine Engines Loads Forces Structural Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |