Blade tip heat transfer and aerodynamics in a large scale turbine cascade with moving endwall
High resolution Nusselt number (Nu) distributions were measured on the blade tip surface of a large, 1.0 meter-chord, low-speed cascade representative of a high-pressure turbine. Data was obtained at a Reynolds number of 4.0 × 105 based on exit velocity and blade axial chord. Tip clearance levels ra...
| Autors principals: | , , , , , |
|---|---|
| Format: | Journal article |
| Idioma: | English |
| Publicat: |
2006
|