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Component specific modeling (Document No: 19870001774)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Roberts, M. L. |
| Copyright Year | 1984 |
| Description | Modern jet engine design imposes extremely high loadings and temperatures on hot section components. A series of interdisciplinary modeling and analysis techniques which were specialized to address three specific components (combustor burner linings, hollow air-cooled turbine blades, and air-cooled turbine vanes) were developed and verified. These techniques will incorporate data as well as theoretical methods from many diverse areas, including cycle and performance analysis, heat transfer analysis, linear and nonlinear stress analysis, and mission analysis. Building on the proven techniques already available in these fields, the new methods developed will be integrated to predict temperature, deformation, stress, and strain histories throughout a complete flight mission. |
| File Size | 363495 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870001774 |
| Archival Resource Key | ark:/13960/t3033pj9k |
| Language | English |
| Publisher Date | 1984-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Temperature Deformation Turbine Blades Engine Design Linings Pressure Distribution Jet Engines Stress-strain Relationships Vanes Mathematical Models Prediction Analysis Techniques Heat Transfer Loads Forces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
