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Measurement of airfoil heat transfer coefficients on a turbine stage (Document No: 19870001788)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Blair, M. F. Dring, R. P. |
| Copyright Year | 1984 |
| Description | The primary basis for heat transfer analysis of turbine airfoils is experimental data obtained in linear cascades. A detailed set of heat transfer coefficients was obtained along the midspan of a stator and a rotor in a rotating turbine stage. The data are to be compared to standard analyses of blade boundary layer heat transfer. A detailed set of heat transfer coefficients was obtained along the midspan of a stator located in the wake of a full upstream turbine stage. Two levels of inlet turbulence (1 and 10 percent) were used. The analytical capability will be examined to improve prediction of the experimental data. |
| File Size | 2413524 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870001788 |
| Archival Resource Key | ark:/13960/t6q001x9t |
| Language | English |
| Publisher Date | 1984-10-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Photography Gas Turbines Rotor Blades Turbomachinery Flow Distribution Stators Airfoils Heat Measurement Heat Transfer Coefficients Prediction Analysis Techniques Boundary Layers 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 | Article |
