Search NASA⌕ Search

NASA NTRS · 19930034755

Heat transfer performance comparisons of five different rectangular channels with parallel angled ribs

Abstract

This paper systematically presents the results of heat transfer and friction factor data measured in five short rectangular channels with turbulence promoters. The project investigated the combined effects of the channel aspect ratio, rib angle-of-attack, and flow Reynolds number on heat transfer and pressure drop in rectangular channels with two opposite ribbed walls. The channel aspect ratio (width-to-height, W/H, ribs on side W) varied from 1/4 to 1/2, to 1, 2, and 4, while the corresponding rib angles-of-attack alpha were 90 deg, 60 deg, 45 deg, and 30 deg, respectively. The Reynolds number range was 10,000-60,000. The results suggest that the narrow aspect ratio channels (W/H less than 1) give much better heat transfer performance than the wide aspect ratio channels (W/H greater than 1). For the square channel (W/H = 1), the 60 deg/45 deg angled ribs provide the best heat transfer performance. For the narrow aspect ratio channel (W/H = 1/4 or 1/2), the 45 deg/60 deg angled ribs are recommended, while the 30 deg/45 deg angled ribs are better for wide aspect ratio channels (W/H = 4 or 2).

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Park, J. S., Han, J. C., Huang, Y., Ou, S., Boyle, R. J.. 1992-11-01. Heat transfer performance comparisons of five different rectangular channels with parallel angled ribs. https://ntrs.nasa.gov/citations/19930034755

Cite the original work for its findings. Save a collection to share your selection of sources.