Efficiency of a thermal screen behind rows of orifices on the leading edge of a gas turbine blade
โ Scribed by V. M. Repukhov; E. N. Zotov
- Publisher
- Springer US
- Year
- 1993
- Tongue
- English
- Weight
- 473 KB
- Volume
- 65
- Category
- Article
- ISSN
- 1573-871X
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๐ SIMILAR VOLUMES
Film cooling of a symmetrical turbine-blade model by lateral and non-lateral injection from one row of holes placed on each side near the leading edge is calculated with a 3D ยฎnite-volume method on multi-block grids. For various blowing rates, the ยฏow and temperature ยฎelds are predicted, and in part
The content of this work is the development and investigation of a high temperature coating system for gas turbine blades. On a single crystal CMSX4 substrate a thin CVD layer of a-alumina is deposited as diffusion barrier coating. As a protection against hightemperature corrosion it is covered with