## Abstract The heat transfer characteristics and flow behavior in a rectangular passage with two opposite 45ยฐ skewed ribs for turbine rotor blade have been investigated for Reynolds numbers from 7800 to 19,000. In this blade, the spanwise coolant passage at the trailing edge region whose thickness
โฆ LIBER โฆ
Heat transfer enhancement in a converging passage with discrete ribs
โ Scribed by Zhengjun Hu; Jiarui Shen
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 822 KB
- Volume
- 39
- Category
- Article
- ISSN
- 0017-9310
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## Abstract Experiments have been performed for turbulent channel flow obstructed with a flat body. The local heat transfer coefficient and the wall static pressure were measured on two kinds of flat bodies for which the trailing edge shape differed. The length of the body, the thickness of the bod