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Burner liner thermal/structural load modelling
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Maffeo, R. J. |
| Copyright Year | 1984 |
| Description | A serious problem exists interfacing the output temperatures and temperature gradients from either the heat transfer codes or engine tests with the input to stress analysis codes. A thermal load transfer code was developed and was used in conjunction with a three-dimensional model of a combustor liner for verification. The 3D heat transfer and stress analysis models of combustor liners and turbine blades were used to validate the mapped temperature produced by the transfer module. Verification cases were made for both finite element and finite difference heat transfer codes. A user manual for the code was written and is available. |
| File Size | 215929 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870001772 |
| Archival Resource Key | ark:/13960/t5k981d9q |
| Language | English |
| Publisher Date | 1984-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Finite Element Method Stress Analysis Temperature Format Coding Transfer Functions Finite Difference Theory Linings Applications Programs Computers Combustion Chambers Three Dimensional Models Heat Transfer Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
