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The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model. volume 3: heat transfer data tabulation 65 percent axial spacing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Blair, M. F. Dring, R. P. Joslyn, H. D. |
| Copyright Year | 1986 |
| Description | This is Volume 3 - Heat Transfer Data Tabulation (65 percent Axial Spacing) of a combined experimental and analytical program which was conducted to examine the effects of inlet turbulence on airfoil heat transfer. The experimental portion of the study was conducted in a large-scale (approximately 5X engine), ambient temperature, rotating turbine model configured in both single stage and stage-and-a-half arrangements. Heat transfer measurements were obtained using low-conductivity airfoils with miniature thermocouples welded to a thin, electrically heated surface skin. Heat transfer data were acquired for various combinations of low or high inlet turbulence intensity, flow coefficient, first-stator/rotor axial spacing, Reynolds number and relative circumferential position of the first and second stators. |
| File Size | 5517662 |
| Page Count | 236 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880019546 |
| Archival Resource Key | ark:/13960/t9770cd6p |
| Language | English |
| Publisher Date | 1986-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Turbulence Thermocouples Rotors Rotor Stator Interactions Skin Structural Member Aerodynamics Airfoils Inlet Flow Unsteady Flow Ambient Temperature Stators Turbines Heat Transfer Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
