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A general method for unsteady stagnation region heat transfer and results for model turbine flows
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cebeci, Tuncer Platzer, Max F. Krainer Sr., Andreas Simoneau, Robert J. |
| Copyright Year | 1987 |
| Description | Recent experiments suggest that the heat-transfer characteristics of stator blades are influenced by the frequency of passing of upstream rotor blades. The calculation of these effects requires that the movement of the stagnation point with variations in freestream velocity is properly represented together with the possible effects of turbulence characteristics on the thin leading-edge boundary layer. A procedure to permit the achievement of these purposes is described for laminar flows in this paper together with results of its application to two model problems which demonstrate its abilities and quantify the influence of wake characteristics on fluid-dynamic and heat-transfer properties of the flow and their effects on surface heat transfer. |
| File Size | 549741 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870007569 |
| Archival Resource Key | ark:/13960/t7bs3pb90 |
| Language | English |
| Publisher Date | 1987-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Fluid Dynamics Laminar Flow Rotor Blades Turbomachinery Stagnation Point Wakes Stator Blades Unsteady Flow Free Flow Leading Edges Turbines 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 | Article |
