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Predicted turbine heat transfer for a range of test conditions
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lucci, B. L. Boyle, R. J. |
| Copyright Year | 1996 |
| Description | Comparisons are shown between predictions and experimental data for blade and endwall heat transfer. The comparisons of computational domain parisons are given for both vane and rotor geometries over an extensive range of Reynolds and Mach numbers. Comparisons are made with experimental data from a variety of sources. A number of turbulence models are available for predicting blade surface heat transfer, as well as aerodynamic performance. The results of an investigation to determine the turbulence model which gives the best agreement with experimental data over a wide range of test conditions are presented. |
| File Size | 2623059 |
| Page Count | 42 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19970007979 |
| Archival Resource Key | ark:/13960/t0wq4wv12 |
| Language | English |
| Publisher Date | 1996-11-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Navier-stokes Equation Turbine Blades Turbulence Models Reynolds Number Rotors Wall Flow Vanes Aerodynamic Characteristics Heat Transfer Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
