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 ®nite-volume method on multi-block grids. For various blowing rates, the ¯ow and temperature ®elds are predicted, and in part
✦ LIBER ✦
Heat transfer enhancement in combined cooling of the turbine blade leading edge
✍ Scribed by A. V. Shchukin; A. V. Il’inkov; S. G. Dezider’ev; S. N. Ivanov
- Book ID
- 124050579
- Publisher
- Allerton Press, Inc.
- Year
- 2013
- Tongue
- English
- Weight
- 366 KB
- Volume
- 56
- Category
- Article
- ISSN
- 1068-7998
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