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Burner liner thermal-structural load modeling
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Maffeo, R. |
| Copyright Year | 1986 |
| Description | The software package Transfer Analysis Code to Interface Thermal/Structural Problems (TRANCITS) was developed. The TRANCITS code is used to interface temperature data between thermal and structural analytical models. The use of this transfer module allows the heat transfer analyst to select the thermal mesh density and thermal analysis code best suited to solve the thermal problem and gives the same freedoms to the stress analyst, without the efficiency penalties associated with common meshes and the accuracy penalties associated with the manual transfer of thermal data. |
| File Size | 7333367 |
| Page Count | 207 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860012461 |
| Archival Resource Key | ark:/13960/t3wt3k201 |
| Language | English |
| Publisher Date | 1986-01-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Temperature Distribution Stress Analysis Transfer Functions Linings Burners Computer Programs Finite Element Method Interfaces Structural Strain Finite Difference Theory Mathematical Models Combustion Chambers Heat Transfer Thermal Stresses Computer Aided Design 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 | Technical Report |
