Measurements of derailed heat transfer coefficients on two principal walls
of a triangular duct with a swirling flow are undertaken by using a transie
nt liquid crystal technique. The vertex corners of the triangular duct are
45, 45, and 90 deg. The swirl-motioned airflow is induced by an array of ta
ngential jets on the side entries. The effects of flow Reynolds number (860
0 less than or equal to Re less than or equal to 21000) and the jet inlet a
ngle (alpha = 75, 45, and 30 deg) ave examined. Flow visualization by using
smoke injection is conducted for better understanding the complicated flow
phenomena in the swirling-flow channel. Results show that the heat transfe
r for alpha = 75 deg is enhanced mainly by the wall jets as well as the imp
inging jets; while the mechanisms of heat heat transfer enhancement for alp
ha = 45 and 30 deg could be characterized as the swirling-flow cooling. On
the bottom wall, jets at a = 75 deg produce the best wall-averaged heat tra
nsfer due to the strongest wall-jet effect among the three angles (alpha) i
nvestigated On the target wall, however, the heat transfer enhancements by
swirling flow (alpha = 45 and 30 deg) are slightly higher than those by imp
inging jets (alpha = 75 deg). Correlations for wall-averaged Nusselt number
Sor the bottom and target walls of the triangular duct are developed in te
rms of the flow Reynolds number for different jet inlet angles.