This paper reports on a three-dimensional study of air through two-row cyli
nder tubes. The analysis is intended to present a comparison of numerical a
nd experimental data to validate the laminar flow postulation. The current
study explores the influence of four perforated fin surfaces on the pressur
e drop and heat transfer rate. To gain further insight into the three dimen
sional vortical flow structure, we conduct a topological study of the veloc
ity field. Examination of the surface flow topology and the flow patterns a
t cross-flow planes sheds some light on the complex interaction of the cyli
nder tube with the mainstream flow. This study clearly reveals a saddle poi
nt in front of the first row of cylinder tubes. Also clearly revealed by th
e computed solutions is a flow reversal found in the wake of the tube. The
character of the critical-point-induced flow is also addressed. This study
shows that the addition of perforated fins is not without deficiency. There
is, in fact a trade-off between the benefit of having an improved heat tra
nsfer and the penalty of having an increased pressure drop.