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3-d inelastic analysis methods for hot section components
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Todd, E. S. |
| Copyright Year | 1985 |
| Description | The objective is to produce a series of new computer codes that permit more accurate and efficient three dimensional inelastic structural analysis of combustor liners, turbine blades, and turbine vanes. Each code embodies a progression of mathematical models for increasingly comprehensive representaion of the geometrical features, loading conditions, and forms of nonlinear material response that distinguish these three groups of hot section components. |
| File Size | 224024 |
| Page Count | 5 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880001783 |
| Archival Resource Key | ark:/13960/t16m84c2q |
| Language | English |
| Publisher Date | 1985-10-01 |
| Access Restriction | Open |
| Subject Keyword | Computer Programming And Software Turbine Blades Gas Turbine Engines Linings Nonlinearity Mathematical Models Combustion Chambers Computer Programs 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 |