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Detailed heat transfer distributions in two-pass square channels with rib turbulators and bleed holes
- Source :
- International Journal of Heat and Mass Transfer; December 1998, Vol. 41 Issue: 23 p3781-3791, 11p
- Publication Year :
- 1998
-
Abstract
- Detailed heat transfer coefficient distributions are presented for a two-pass square channel with a 180° turn. One wall of the channel has periodically placed rib turbulators and bleed holes. Four different configurations of 90° parallel, 60° parallel, 60° V ribs, and 60° inverted V ribs are studied in conjunction with the effect of bleed holes on the same wall. The surface is coated with a thin layer of thermochromic liquid crystals and a transient test is run to obtain the detailed heat transfer distributions. Detailed distributions show distinctive peaks in heat transfer levels around bleed holes and on rib turbulator tips. The 60° parallel, 60° V, and 60° inverted V ribbed channels produce similar levels of heat transfer enhancement in the first pass. However, the 60° inverted V ribbed channel produces higher enhancement in the second pass. Regional-averaged heat transfer results indicate that a surface with bleed holes provides similar heat transfer enhancement as that for a surface without bleed holes although 20–25% of the inlet mass flow exits through the bleed holes.
Details
- Language :
- English
- ISSN :
- 00179310
- Volume :
- 41
- Issue :
- 23
- Database :
- Supplemental Index
- Journal :
- International Journal of Heat and Mass Transfer
- Publication Type :
- Periodical
- Accession number :
- ejs2531288
- Full Text :
- https://doi.org/10.1016/S0017-9310(98)00099-4