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Component-specific modeling (Document No: 19850023806)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McKnight, R. L. |
| Copyright Year | 1985 |
| Description | Accomplishments are described for the second year effort of a 3-year program to develop methodology for component specific modeling of aircraft engine hot section components (turbine blades, turbine vanes, and burner liners). These accomplishments include: (1) engine thermodynamic and mission models; (2) geometry model generators; (3) remeshing; (4) specialty 3-D inelastic stuctural analysis; (5) computationally efficient solvers, (6) adaptive solution strategies; (7) engine performance parameters/component response variables decomposition and synthesis; (8) integrated software architecture and development, and (9) validation cases for software developed. |
| File Size | 3658792 |
| Page Count | 132 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850023806 |
| Archival Resource Key | ark:/13960/t41s1pg5g |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Stress-strain Relationships Turbine Blades Deformation Architecture Computers Aircraft Engines Thermodynamic Properties Engine Parts Prediction Analysis Techniques Turbine Engines 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 | Technical Report |