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A general method for unsteady heat transfer on turbine blades
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cebeci, Tuncer Platzer, Max F. |
| Copyright Year | 1989 |
| Description | The development of a general method for calculating unsteady heat transfer on turbine blades is described. It is based on the numerical solution of the boundary-layer equations for laminar, transitional, and turbulent flows. A novel procedure has been developed to account for the movement of the stagnation point caused by blade-passing wakes and has been applied to the stagnation region of three model flows with results which confirm its validity for laminar flows. It has also been applied to an experimental arrangement in which the average Nusselt number has been reported for turbulent flows and the results show considerable promise. |
| File Size | 1344832 |
| Page Count | 39 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890005998 |
| Archival Resource Key | ark:/13960/t4cp2110t |
| Language | English |
| Publisher Date | 1989-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Fluid Mechanics Nusselt Number Turbine Blades Laminar Flow Stagnation Point Wakes Unsteady Flow Heat Transfer Boundary Layers 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 |
